WO2009066183A2 - Tightly-coupled pcb gnss circuit and manufacturing method - Google Patents

Tightly-coupled pcb gnss circuit and manufacturing method Download PDF

Info

Publication number
WO2009066183A2
WO2009066183A2 PCT/IB2008/003796 IB2008003796W WO2009066183A2 WO 2009066183 A2 WO2009066183 A2 WO 2009066183A2 IB 2008003796 W IB2008003796 W IB 2008003796W WO 2009066183 A2 WO2009066183 A2 WO 2009066183A2
Authority
WO
WIPO (PCT)
Prior art keywords
pcb
receiver
decoupling
circuit
antenna
Prior art date
Application number
PCT/IB2008/003796
Other languages
French (fr)
Other versions
WO2009066183A3 (en
Inventor
Andrew J. Jakab
Nicholas J. Boorman
Original Assignee
Hemisphere Gps Llc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hemisphere Gps Llc filed Critical Hemisphere Gps Llc
Publication of WO2009066183A2 publication Critical patent/WO2009066183A2/en
Publication of WO2009066183A3 publication Critical patent/WO2009066183A3/en

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/12Supports; Mounting means
    • H01Q1/22Supports; Mounting means by structural association with other equipment or articles
    • H01Q1/24Supports; Mounting means by structural association with other equipment or articles with receiving set
    • H01Q1/241Supports; Mounting means by structural association with other equipment or articles with receiving set used in mobile communications, e.g. GSM
    • H01Q1/242Supports; Mounting means by structural association with other equipment or articles with receiving set used in mobile communications, e.g. GSM specially adapted for hand-held use
    • H01Q1/243Supports; Mounting means by structural association with other equipment or articles with receiving set used in mobile communications, e.g. GSM specially adapted for hand-held use with built-in antennas
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/36Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith
    • H01Q1/38Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith formed by a conductive layer on an insulating support
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/52Means for reducing coupling between antennas; Means for reducing coupling between an antenna and another structure
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K1/00Printed circuits
    • H05K1/02Details
    • H05K1/0213Electrical arrangements not otherwise provided for
    • H05K1/0216Reduction of cross-talk, noise or electromagnetic interference
    • H05K1/023Reduction of cross-talk, noise or electromagnetic interference using auxiliary mounted passive components or auxiliary substances
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K1/00Printed circuits
    • H05K1/02Details
    • H05K1/0213Electrical arrangements not otherwise provided for
    • H05K1/0216Reduction of cross-talk, noise or electromagnetic interference
    • H05K1/023Reduction of cross-talk, noise or electromagnetic interference using auxiliary mounted passive components or auxiliary substances
    • H05K1/0231Capacitors or dielectric substances
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K1/00Printed circuits
    • H05K1/02Details
    • H05K1/0213Electrical arrangements not otherwise provided for
    • H05K1/0237High frequency adaptations
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K2201/00Indexing scheme relating to printed circuits covered by H05K1/00
    • H05K2201/09Shape and layout
    • H05K2201/09818Shape or layout details not covered by a single group of H05K2201/09009 - H05K2201/09809
    • H05K2201/09972Partitioned, e.g. portions of a PCB dedicated to different functions; Boundary lines therefore; Portions of a PCB being processed separately or differently
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49002Electrical device making
    • Y10T29/49016Antenna or wave energy "plumbing" making
    • Y10T29/49018Antenna or wave energy "plumbing" making with other electrical component

Definitions

  • the present invention relates generally to printed circuit boards (PCBs). and in particular to a tightly-coupled PCB for mounting one or mo e receivers with multiple. independent radio frequency (RF) front ends in close p ⁇ o ⁇ ir iity to multiple, respective antennas.
  • the circuit is noise-filtered by electrically decoupling and i; dating the conductive reference planes of the PCB.
  • Ty pical PCB construction comprises one or more reference lay ers, which can prov ide power and ground (common) planar sources for the entire circuit.
  • Component conductors are connected to the reference layers as required for their operation.
  • Other I ⁇ yers conduct signals, and can be photo-etched with trace conductors linking other componeni conductors.
  • microstrip traces can be mounted on the PCB surfaces or w ithin the PCB layers for electrically coupling components.
  • Signal noise control represents a significant aspe ct of PCB circuit design.
  • Such considerations are particularly significant in designing circi its with RF receiver and antenna components, because circuit noise from switching components, power sources, "skin effect" conductivity and other noise-producing elements can significantly interfere with the reception and processing of transmitted signals.
  • GNSS global lav igation satellite s>stem
  • GPS global positioning system
  • receivers operate in the microw ave frequency range, whose high frequencies tend to increase noise-related recepi ion problems and signal interference.
  • such systems are susceptible to multipath signal phenomena, which tend to reduce s> stem accuracy and performance.
  • a prc ⁇ ions solution has been to physically isolate the receiver and antenna components, w hich can be connected by a shielded RF cabl :.
  • it is often more cost- effective to mount as many system components as possible MI a single PCB.
  • locating the receiver and its anlenna(s) in close proximity tends to improve peiformance by eliminating relatively lengthy RF connecting cables, prov ided the potenlial for noise interference can be controlled.
  • Smart antennas combining antennas and recen ers at single locations have previously been utilized, but do not electrically decouple the circuit components or utilize the ground reference planes for additional antenna area.
  • the design criteria lor GNSS receiver antenna PCBs would preferably included minimizing overall size, placing the receiver and antenna components in close proximity, accommodating multiple antennas and controllir g signal noise.
  • Prev ious receiver- antenna PCBs and manufacturing methods have not provide il the advantages and features of the present invention.
  • a PCB is designed in a manner to isolate and control the inter-frequenc_ ⁇ noise sources, and piovides for the use of components for decoupling reference lavers thereof, which can further separate and decouple lhe ground planes.
  • a receiver w ith multiple, independent RF front end components can be mounted on the PCB in close pro ⁇ imitv to multiple antennas.
  • the receiver and ante nnas are connected b> optimized transmission lines embedded within the PCB between the ground planes, or bv surface microstrip antenna traces. The impedance of the transmission lines is controlled during the process of manufacturing the PCB.
  • Fig. 1 is a schematic diagram of a tightly -coupled PCB circuit embodying an aspect of the present invention w ith a receiver and a pair of antennas located in proximity and trace- connected to each other on the PCB.
  • Fig. 2 is a schematic diagram of another tightK-eoupled PCB circuit embod> ing another aspect of the present invention with three antennas I race-connected to a receiver on a single PCB.
  • FIG. 3 is a top schematic diagram of another tigh tly -coupled PCB embodying another aspect of the present invention w ith a modified line of decoupling capacitors.
  • Fig. 4 is a bottom schematic diagram thereof.
  • Fig. 5 is a top schematic diagram of another tightly-coupled PCB embodying another aspect of the present invention with a modified configuration and lav out.
  • Fig. 6 is a bottom schematic diagram thereof. DETAILED DESCRIPTION OF THE PREFEKRED EMBODIMENTS
  • the reference numeral 2 generally designates a tightly-coupled printed circuit board (PCB) circuit embodying an aspect of the present invention.
  • PCB printed circuit board
  • the circuit 2 includes a pair of antennas 4 coupled to a sensing receiver 6.
  • the receiver 6 can comprise a GNSS (e.g.. GPS) receiver operating in the microwave frequency range.
  • the antennas 4 and the receiver 6 are mounted on a multi-layer PCB 8, w hich can
  • the conductive layers can include reference layers adapted for powering the circuit 2 via a positive, power layer and one or more groiinc or common lavers providing a ground plane(s) for the circuit.
  • the PCB 8 can also include one or more signal layers, w hich can be photo-etched in a suitable circuit diagram partem(s) for t lectricalK coupling the circuit 5 components.
  • the antennas 4 and the receiver ⁇ can be connected by RF transmission striplines or traces 10.
  • w hich can be either embedded within the PCB 8 and shielded between the reference layers thereof in a sandwiching construction, or located on the PCB 8 surface and comprise surface microstrip antenna trac es. I f surface-mounted, the RF transmission striplines I O would be bottom-shielded by the lop la ⁇ er of the PCB 8.
  • I O of the RF transmission striplines I O is preferably optimized by controlling impedance (Z), e.g. b> v ary ing the thickness of the traces 10.
  • decouplers 12 form decoupling lines. 1 -. which extend from the receiver 6 to respective ends 16 of the PCB 8.
  • the lines 14 include bends 1 8 and form grounded isolation islands 20 which are relatively noise-free b> virtue of the electrical decoupling function of the
  • the RF inputs via the antennas 4 are near thi: ends 16 of the PCB 8.
  • the decoupling lines 14 can be formed with bends and other configurations as necessary in order to locate the RF input signals as close as possible to the physiuil RF connectors from within the RF transmission striplines 1 0 in order to provide optimal RF signal paths from the antennas 4 to the receiver 6.
  • the decouplers 12 can comprise capacitors, resistors or inductors, w hich are chosen
  • the configurations and locations of the isolation islands 20 w ithm the PCB also provide impedance control, in conjunction w ith the decoupling lines 14 and the operating parameters of the circuit 2.
  • Such operating parameters can include such variables as poiver, voltage, current, frequency and amplitude of the signals encountered bv the components of lhe circuit 2. including the operating ranges of such parameters.
  • Multiple different capacitive values of the decouplers 12 can be utilized to filter specific frequencies between the decoupled component ground planes.
  • the decouplers 12 and the isolation islands 20 preferably extend between, yet still allow, electrical connections between the reference layers (e.g., ground planes and/or positive reference la>er) of the PCB 8.
  • the respective independent ground planes of the circuit components, such as the antennas 4. the receiver 6 and the HF transmission lines 10 are electrically decoupled by the decouplers 12.
  • a relatively large area of isolation is preferably formed in the PCB 8 by the isolation islands 20 in order to maximize the signal noise-isolating operation of the decoupling lines 14.
  • the PCB circuit 2 can encounter nc ise and electrical interference from a variety of interna! and external sources.
  • High-frequency receivers, such as those utilized in GNSS (e.g., GPS). are somewhat susceptible to degradation of performance due to such interference, with the potential for resulting inaccuracies in their positioning functions.
  • the isolation islands 20 tend to be relatively free of such noise signals whereby the antennas 4 can be located relatively close to the receiver 6 without being subj ected to excessive noise.
  • decoupling the PCB circuit 2 Another benefit of decoupling the PCB circuit 2 is that the need for sophisticated filtering and processing functions, which are commonly performed by processors u>ing Kalman and other filtering software techniques, can be eliminated or at least reduced.
  • a further advantage of the decoupled PCB circuit 2 is that the PCB ground planes provide additional antenna areas for increasing the effectiveness of the antennas 4. Still further, the additional costs associated w ith separate circuit boards and standalone components can be avoided by utilizing the decoupled PCB 8. III. First Alternative Aspect Tightly-Coupled PCB Circuit : ; 2
  • a tightl ⁇ -coupled PCB circuit 52 comprising a first alternative aspect or embodiment of the present invention is shown in Fig. 2 and includes an additional antenna 4.
  • Such three- antenna GNSS receiver circuits can be utilized in vehicle guidance s ⁇ stems and machine control applications and are capable of determining vehicle and eqi ipment attitude with respect to three axes.
  • a PCB 58 can be alternative y configured for the third antenna 4 and can assume various other alternative configurations for additional components, including additional antennas, receivers, etc. Still further, additional circuits can be placed on PCBs which are tightlv -coupled and create isolation islands according to the present invention.
  • the tightly- coupled decoupled PC B circuit 52 includes decoupling line-, 64 of decouplers 62, which fo ⁇ n
  • a tightly-coupled PCB circuit 102 comprising a second alternative aspect or embodiment of the present invention is shown in Figs. 3 an J 4 and includes a PCB 103.
  • the PCB circuit 102 includes a receiver 104.
  • Multiple decoupling capacitors 1 12 form first and second decoupling lines 1 14. 1 16.
  • first and second RF striphnes or traces 121 , 122 are surface- mounted on the bottom surface of the PCB 103 and extend iom the receiver 104 to the antennas 106, 108 respectively.
  • a tightly-coupled PCB circuit 152 comprising a third alternative aspect or embodiment of the present invention is shown in Figs. 5 and 6 and includes a PCB 153.
  • the PCB circuit 152 includes a receiver 154.
  • a central isolation island 169 is formed for the receiver 154 and a power supply 160. As shown in Figs.
  • the isolation island 169 can have an irregular shape.
  • Internal first and second RF striplines or traces 1 71 , 172 are provided w ithin the PCB 153 and extend from the central isolation island 169 to the antennas 156. 158 located in the isolation islands 168. 1 70 respectively.
  • the R F traces 1 71. 172 can be surface- mounted.
  • the invention can be embodied in various forms, and is not to be limited to the examples discussed above.
  • the PCBs and the isolation islands can be formed in a variety of configurations.
  • various components can be assembled in different configurations to form a wide variety of PCB circuits, which can effectively utilize the closely-coupled construction of the present invention w ith isolation islands.
  • multiple antennas and receivers can be provided.
  • GNSS receivers and patch antennas are shown, other RF receivers and antennas can be utilized.
  • the range of components and conf ⁇ gLirations w hich can be utilized in the practice of the present invention is ⁇ irtualk unlimited.

Abstract

A tightly-coupled printed circuit board (PCB) circuit includes components mounted on a PCB enabling smaller integrations using decoupled lines extending between reference layers, such as ground planes, which lines form isolation islands on the PCB. The decouplers are capacitors, inductors and/or resistors in tandem with ground layers of the PCB. The isolated components can comprise high-frequency RF antennas and receivers, for example in a GNSS antenna-receiver circuit. Multiple antennas can be connected to one or more receivers with multiple, independent RF front end components by RF traces, which are either embedded within the PCB.

Description

TIGHTLY-COUPLED PCB GNSS CIRCUIT AND MANUFACTURING METHOD
CROSS-REFERENCE TO RELATED APPLICATION
[0001] This application claims the benefit of U.S. Patent Application Serial No.
12/239.312. filed September 26, 2008. which claims the benefit of U.S. Provisional Application No. 60/975.727. filed September 27. 2007, which are incorporated herein by reference.
BACKGROUND OF THE INVENTION
1. Field of the Invention
[0002] The present invention relates generally to printed circuit boards (PCBs). and in particular to a tightly-coupled PCB for mounting one or mo e receivers with multiple. independent radio frequency ( RF) front ends in close pιo\ir iity to multiple, respective antennas. The circuit is noise-filtered by electrically decoupling and i; dating the conductive reference planes of the PCB.
2. Description of the Related Art
[0003] PCB manufacturing techniques are well-developed and enable the cost-effective production of circuits w ith virtual ly unlimited configuratior s and combinations of components. Ty pical PCB construction comprises one or more reference lay ers, which can prov ide power and ground (common) planar sources for the entire circuit. Component conductors are connected to the reference layers as required for their operation. Other I∑ yers conduct signals, and can be photo-etched with trace conductors linking other componeni conductors. Still further, microstrip traces can be mounted on the PCB surfaces or w ithin the PCB layers for electrically coupling components.
[0004] Signal noise control represents a significant aspe ct of PCB circuit design. Such considerations are particularly significant in designing circi its with RF receiver and antenna components, because circuit noise from switching components, power sources, "skin effect" conductivity and other noise-producing elements can significantly interfere with the reception and processing of transmitted signals. For example, global lav igation satellite s>stem (GNSS. including global positioning system (GPS)) receivers operate in the microw ave frequency range, whose high frequencies tend to increase noise-related recepi ion problems and signal interference. For example, such systems are susceptible to multipath signal phenomena, which tend to reduce s> stem accuracy and performance.
[0005| A prc\ ions solution has been to physically isolate the receiver and antenna components, w hich can be connected by a shielded RF cabl :. However, it is often more cost- effective to mount as many system components as possible MI a single PCB. Moreover, locating the receiver and its anlenna(s) in close proximity tends to improve peiformance by eliminating relatively lengthy RF connecting cables, prov ided the potenlial for noise interference can be controlled. "Smart" antennas combining antennas and recen ers at single locations have previously been utilized, but do not electrically decouple the circuit components or utilize the ground reference planes for additional antenna area. [0006| Therefore, the design criteria lor GNSS receiver antenna PCBs would preferably included minimizing overall size, placing the receiver and antenna components in close proximity, accommodating multiple antennas and controllir g signal noise. Prev ious receiver- antenna PCBs and manufacturing methods have not provide il the advantages and features of the present invention.
-J-
SUMMARY OF THE INVENTION
[0007] In the practice of an aspect of the present invention, a PCB is designed in a manner to isolate and control the inter-frequenc_\ noise sources, and piovides for the use of components for decoupling reference lavers thereof, which can further separate and decouple lhe ground planes. A receiver w ith multiple, independent RF front end components can be mounted on the PCB in close proλimitv to multiple antennas. The receiver and ante nnas are connected b> optimized transmission lines embedded within the PCB between the ground planes, or bv surface microstrip antenna traces. The impedance of the transmission lines is controlled during the process of manufacturing the PCB.
BRIEF DESCRIPTION OF THE DRAWINGS
[0008] Fig. 1 is a schematic diagram of a tightly -coupled PCB circuit embodying an aspect of the present invention w ith a receiver and a pair of antennas located in proximity and trace- connected to each other on the PCB. [0009] Fig. 2 is a schematic diagram of another tightK-eoupled PCB circuit embod> ing another aspect of the present invention with three antennas I race-connected to a receiver on a single PCB.
[00010] Fig. 3 is a top schematic diagram of another tigh tly -coupled PCB embodying another aspect of the present invention w ith a modified line of decoupling capacitors. [00011] Fig. 4 is a bottom schematic diagram thereof.
[00012] Fig. 5 is a top schematic diagram of another tightly-coupled PCB embodying another aspect of the present invention with a modified configuration and lav out. [00013] Fig. 6 is a bottom schematic diagram thereof. DETAILED DESCRIPTION OF THE PREFEKRED EMBODIMENTS
I . Introduction and Environment
|00014] As required, detailed embodiments of the preseni invention are disclosed herein: 5 however, it is to be understood that the disclosed embodime nts are merely exemplar) of the invention, which may be embodied in various forms. There fore, specific structural and functional details disclosed herein are not to be interpreted ;ιs limiting, but merely as a basis for the claims and as a representative basis for teaching one skil led in the art to variously employ the present invention in virtually any appropriately detailed structure.
I O [00015] Certain terminology will be used in the follow ing description for convenience in reference only and w ill not be limiting. For example, up. down, front, back, right and left refer to the invention as oriented in the view being referred to. The words "inwardly" and "outwardly " refer to directions toward and away from, respectively, the .'.eometric center of the embodiment being described and designated parts thereof. Said terminology w ill include the words
15 specifically mentioned, derivatives thereof and words of similar meaning.
II. Tightly-Coupled PCB Circuit 2
[00016] Referring to Fig. 1 of the draw ings in more detail, the reference numeral 2 generally designates a tightly-coupled printed circuit board (PCB) circuit embodying an aspect of the present invention. Without limitation on the generality of tightly-coupled PCB circuits for
20 which the present invention can be advantageously applied, the circuit 2 includes a pair of antennas 4 coupled to a sensing receiver 6. By way of example and without limitation, the receiver 6 can comprise a GNSS (e.g.. GPS) receiver operating in the microwave frequency range. |00017] The antennas 4 and the receiver 6 are mounted on a multi-layer PCB 8, w hich can
25 include multiple conductive layers separated by insulating layers foπned of epoxy or other suitable material. The conductive layers can include reference layers adapted for powering the circuit 2 via a positive, power layer and one or more groiinc or common lavers providing a ground plane(s) for the circuit. The PCB 8 can also include one or more signal layers, w hich can be photo-etched in a suitable circuit diagram partem(s) for t lectricalK coupling the circuit 5 components. For example, the antennas 4 and the receiver ό can be connected by RF transmission striplines or traces 10. w hich can be either embedded within the PCB 8 and shielded between the reference layers thereof in a sandwiching construction, or located on the PCB 8 surface and comprise surface microstrip antenna trac es. I f surface-mounted, the RF transmission striplines I O would be bottom-shielded by the lop la\er of the PCB 8. The function
I O of the RF transmission striplines I O is preferably optimized by controlling impedance (Z), e.g. b> v ary ing the thickness of the traces 10.
[00018] Multiple decouplers 12 form decoupling lines. 1 -. which extend from the receiver 6 to respective ends 16 of the PCB 8. The lines 14 include bends 1 8 and form grounded isolation islands 20 which are relatively noise-free b> virtue of the electrical decoupling function of the
15 decouplers 12. The RF inputs via the antennas 4 are near thi: ends 16 of the PCB 8. The decoupling lines 14 can be formed with bends and other configurations as necessary in order to locate the RF input signals as close as possible to the physiuil RF connectors from within the RF transmission striplines 1 0 in order to provide optimal RF signal paths from the antennas 4 to the receiver 6. The decouplers 12 can comprise capacitors, resistors or inductors, w hich are chosen
20 for impedance control based on characteristics and operating parameters of the circuit 2. The configurations and locations of the isolation islands 20 w ithm the PCB also provide impedance control, in conjunction w ith the decoupling lines 14 and the operating parameters of the circuit 2. Such operating parameters can include such variables as poiver, voltage, current, frequency and amplitude of the signals encountered bv the components of lhe circuit 2. including the operating ranges of such parameters. Multiple different capacitive values of the decouplers 12 can be utilized to filter specific frequencies between the decoupled component ground planes. |00019] The decouplers 12 and the isolation islands 20 preferably extend between, yet still allow, electrical connections between the reference layers (e.g., ground planes and/or positive reference la>er) of the PCB 8. The respective independent ground planes of the circuit components, such as the antennas 4. the receiver 6 and the HF transmission lines 10 are electrically decoupled by the decouplers 12. A relatively large area of isolation is preferably formed in the PCB 8 by the isolation islands 20 in order to maximize the signal noise-isolating operation of the decoupling lines 14. [00020] In operation, the PCB circuit 2 can encounter nc ise and electrical interference from a variety of interna! and external sources. High-frequency receivers, such as those utilized in GNSS (e.g., GPS). are somewhat susceptible to degradation of performance due to such interference, with the potential for resulting inaccuracies in their positioning functions. The isolation islands 20 tend to be relatively free of such noise signals whereby the antennas 4 can be located relatively close to the receiver 6 without being subj ected to excessive noise.
[00021| The relatively close proximities of the antennas 4 to the receiver 6 tend to minimize signal delays and electromagnetic interference (EMI) probl ems, which can be associated with greater separation and correspondingly longer RF connecting leads. Noise from such signal sources as multipath signals. PCB skin effect, power source fluctuations, phase noise and EMI in general tend to be effectively dissipated by the impedance (capacitive, inductive and/or resistive) of the decouplers 12. Effective decoupling improves signal quality from the antennas 4 to the receiver 6. In the case of GNSS systems, greater positioning accuracy can be achieved. Another benefit of decoupling the PCB circuit 2 is that the need for sophisticated filtering and processing functions, which are commonly performed by processors u>ing Kalman and other filtering software techniques, can be eliminated or at least reduced. A further advantage of the decoupled PCB circuit 2 is that the PCB ground planes provide additional antenna areas for increasing the effectiveness of the antennas 4. Still further, the additional costs associated w ith separate circuit boards and standalone components can be avoided by utilizing the decoupled PCB 8. III. First Alternative Aspect Tightly-Coupled PCB Circuit :;2
5 |00022] A tightl} -coupled PCB circuit 52 comprising a first alternative aspect or embodiment of the present invention is shown in Fig. 2 and includes an additional antenna 4. Such three- antenna GNSS receiver circuits can be utilized in vehicle guidance s\ stems and machine control applications and are capable of determining vehicle and eqi ipment attitude with respect to three axes.
I U [00023] As show n in Fig. 2. a PCB 58 can be alternative y configured for the third antenna 4 and can assume various other alternative configurations for additional components, including additional antennas, receivers, etc. Still further, additional circuits can be placed on PCBs which are tightlv -coupled and create isolation islands according to the present invention. The tightly- coupled decoupled PC B circuit 52 includes decoupling line-, 64 of decouplers 62, which foπn
15 isolation islands 70 in w hich the antennas 4 are mounted in relatively noise-free isolation. Considerable cost sav ings can be achieved using the tight coupling of the present invention because the PCBs can be made smaller and components can be combined on single PCBs to form circuits that might have otherw ise required physical isolation and separation among different components of a circuit.
20 IV. Second Alternative Aspect Tightlv -Coupled PCB Circuit 102
|00024] A tightly-coupled PCB circuit 102 comprising a second alternative aspect or embodiment of the present invention is shown in Figs. 3 an J 4 and includes a PCB 103. The PCB circuit 102 includes a receiver 104. first and second GNSS antennas 106, 108 and a power suppl) 1 10. Multiple decoupling capacitors 1 12 form first and second decoupling lines 1 14. 1 16.
25 which generallj extend in opposite directions from the receiver 104 towards respective ends of the PCB 103 and define respective isolation islands 1 18. 12 ) for the antennas 106. 108 respectively. As shown in Fig. 4. first and second RF striphnes or traces 121 , 122 are surface- mounted on the bottom surface of the PCB 103 and extend iom the receiver 104 to the antennas 106, 108 respectively. V. Third Alternative Aspect Tightly-Coupled PCB Circuit 1 52
[00025] A tightly-coupled PCB circuit 152 comprising a third alternative aspect or embodiment of the present invention is shown in Figs. 5 and 6 and includes a PCB 153. The PCB circuit 152 includes a receiver 154. first and second G MSS patch antennas 156, 158 and a power supply 160. Multiple decoupling capacitors 162 torn first and second decoupling lines 164. 166. w hich form generally circular isolation islands 168. 1 70 at respective ends of the PCB 153 for the antennas 156, 158 respectiv ely. Additional decoupling capacitors 162 are provided adjacent to edges of the PCB 153. A central isolation island 169 is formed for the receiver 154 and a power supply 160. As shown in Figs. 5 and 6, the isolation island 169 can have an irregular shape. Internal first and second RF striplines or traces 1 71 , 172 are provided w ithin the PCB 153 and extend from the central isolation island 169 to the antennas 156. 158 located in the isolation islands 168. 1 70 respectively. Alternatively, the R F traces 1 71. 172 can be surface- mounted.
|00026] It is to be understood that the invention can be embodied in various forms, and is not to be limited to the examples discussed above. For example, the PCBs and the isolation islands can be formed in a variety of configurations. Moreover, various components can be assembled in different configurations to form a wide variety of PCB circuits, which can effectively utilize the closely-coupled construction of the present invention w ith isolation islands. For example, multiple antennas and receivers can be provided. Although GNSS receivers and patch antennas are shown, other RF receivers and antennas can be utilized. The range of components and confϊgLirations w hich can be utilized in the practice of the present invention is \ irtualk unlimited.

Claims

CLAIMSHaving thus described the invention, w hat is claimed as new and desired to be secured by Letters Patent is:
1 . A method of tightly coupling a printed circuit board ( PCB). which method 5 comprises the steps of: providing a PCB w ith multiple conductive layers; separating said conductive layers with insu lating layers: providing a positive reference layer; providing a ground plane comprising a grounded reference la\ er: I O providing a signal lay er; photoetching the signal layer to define a circuit: providing electrical components: connecting each electrical component to one or more layers: forming a decoupling line in said PCB; and 1 5 forming an electrical isolation island in said PCB with said decoupling line.
2. The method of claim I w herein one ot said components comprises a receiver, which method includes the additional steps of: providing said PCB w ith a perimeter: connecting said receiver to said PCB; and 0 extending said decoupl ing line from said receiver to F1CB perimeter.
3. The method of claim 2 w herein said components include an antenna, w hich method includes the additional steps of: providing an RF transm ission line connecting said antenna to said receiver; and 25 locating said antenna in said isolation island.
4. The method of claim 3. w hich include -; the additional steps of: - I I - forming an optimal RF path from the antenna to the receiver, thereby creating a decoupling line: and forming said isolation island along said decoupling line path.
5. The method of claim 2, which includes the additional steps of: locating said receiver in an interior area of said PCB: providing a pair of said decoupling lines: and extending said decoupling lines from said receiver to said PCB perimeter.
6. The method of claim I . which include:; the additional step of:
forming said decoupling line with a plurality of discrete decouplers each extending through said PCB la>ers.
7. The method of claim 3. which includes the additional steps of:
providing said PCB v\ ith three sections each teπninat ng at an outer end:
locating said receiver centrally with said PCB section:; extending outwardly therefrom:
mounting an antenna in each of said sections in proxi nity to its outer end;
extending a pair of said decoupling lines from said receiver to each said PCB section outer end: and
formin 'ag an isolation island in each said PCB section with said antenna located therein.
8. A method of manufacturing a tightly-coupled PCB circuit w ith a power suppl) . a GNSS receiver and first and second GNSS antennas, w hich method comprises the steps of:
providing a PCB with multiple conductive layers: separating said conductive layers with insulating layers: providing a positive reference layer: prov iding a ground plane comprising a giounded reference layer: prov iding a signal layer; photoetching the signal la>er to define a circuit; prov iding said PCB with a perimeter; mounting said power supply and said GNSS receiver .MI said PCB- connecting said power supply and said GNSS receive to said positive and grounded reference layers; prov iding multiple decoupling capacitors; connecting each said capacitors to multiple said PCB layers and electrically closely- coupling said PCB layers with said capacitors; determining optimal first and second RF paths from the antennas to the receiver; aligning multiple said decoupling capacitors along said optimal RF paths and thereb> creating first and second decoupling lines each extending from said receiver to said PCB edge in proximity to a respective antenna; forming first and second isolation islands along said Irst and second decoupling line paths respectively; prov iding first and second RF transmission lines connecting said receiver to said first and second antennas respectively ; and locating said first and second antennas in said first and second isolation islands respectively .
9. A tightly -coupled printed circuit board (PCB) circuit, which includes: multiple conductive layers; insulating layers separating said conductive lay ers, a positive reference layer: a ground plane comprising a grounded reference lay ei : a signal layer: a circuit photoetched in the signal layer; multiple electrical components each connected to one or more lavers: a decoupling line in said PCB: and an electrical isolation island formed by said decoupling line in said PCB.
10. The circuit of claim 9, which includes one of said components comprising a receiver: said PCB including a perimeter: said receiver being connected to said PCB: and said decoupling line extending from said receiver to said PCB perimeter
1 1 . The circuit of claim 10, which includes: said components including an antenna located in said isolation island: and an RF transmission line connecting said antenna to said receiver.
12. The circuit of claim 1 1. which includes: an optimal RF path from the antenna to the receiver, said decoupling line generally follow ing said optimal RF path; and said isolation island being formed along said decoupl ng line path.
13. The circuit of claim 10. w hich includes: said receiver being located in an interior area of said I 'CB: a pair of said decoupling lines: and said decoupling lines extending from said receiver to said PCB perimeter.
14. The circuit of claim 9. which include-.:
said decoupling line being formed with a plurality of discrete decouplers each extending through said PCB la\ ers.
15. The circuit of claim 1 1 , which includes:
said PCB havin« three sections each terminating at an outer end: said receiver being located centrally \\ iih said PCB sections extending outwardly therefrom;
three antennas each mounted in a respective section in proximity to its outer end;
a pair of said decoupling l ines each extending from si iό receiver to a respective PCB section outer end; and
three said isolation islands each located in a respective PCB section and each having a respective antenna located therein.
PCT/IB2008/003796 2007-09-27 2008-09-28 Tightly-coupled pcb gnss circuit and manufacturing method WO2009066183A2 (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US97572707P 2007-09-27 2007-09-27
US60/975,727 2007-09-27
US12/239,312 US7948769B2 (en) 2007-09-27 2008-09-26 Tightly-coupled PCB GNSS circuit and manufacturing method
US12/239,312 2008-09-26

Publications (2)

Publication Number Publication Date
WO2009066183A2 true WO2009066183A2 (en) 2009-05-28
WO2009066183A3 WO2009066183A3 (en) 2011-04-28

Family

ID=40507625

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/IB2008/003796 WO2009066183A2 (en) 2007-09-27 2008-09-28 Tightly-coupled pcb gnss circuit and manufacturing method

Country Status (2)

Country Link
US (1) US7948769B2 (en)
WO (1) WO2009066183A2 (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9002566B2 (en) 2008-02-10 2015-04-07 AgJunction, LLC Visual, GNSS and gyro autosteering control
US9880562B2 (en) 2003-03-20 2018-01-30 Agjunction Llc GNSS and optical guidance and machine control
USRE47055E1 (en) 2009-01-17 2018-09-25 Agjunction Llc Raster-based contour swathing for guidance and variable-rate chemical application
USRE47101E1 (en) 2003-03-20 2018-10-30 Agjunction Llc Control for dispensing material from vehicle
USRE47648E1 (en) 2009-09-17 2019-10-15 Agjunction Llc Integrated multi-sensor control system and method
USRE48527E1 (en) 2007-01-05 2021-04-20 Agjunction Llc Optical tracking vehicle control system and method

Families Citing this family (51)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8334758B2 (en) * 2009-04-13 2012-12-18 Flextronics Automotive, Inc. LIN BUS remote control system
JP5599472B2 (en) * 2009-12-30 2014-10-01 タイコ エレクトロニクス サービス ゲーエムベーハー Antenna device with frequency dependent connection to electrical ground
US8816912B2 (en) 2009-12-30 2014-08-26 Tyco Electronics Services Gmbh Antenna devices having frequency-dependent connection to electrical ground
US10608348B2 (en) 2012-03-31 2020-03-31 SeeScan, Inc. Dual antenna systems with variable polarization
WO2014040250A1 (en) * 2012-09-13 2014-03-20 Telefonaktiebolaget L M Ericsson (Publ) Method and apparatus for antenna calibration
US10490908B2 (en) 2013-03-15 2019-11-26 SeeScan, Inc. Dual antenna systems with variable polarization
US10317512B2 (en) 2014-12-23 2019-06-11 Infineon Technologies Ag RF system with an RFIC and antenna system
US10725150B2 (en) 2014-12-23 2020-07-28 Infineon Technologies Ag System and method for radar
US10615499B2 (en) * 2015-01-14 2020-04-07 Skywave Mobile Communications Inc. Dual role antenna assembly
US9521678B2 (en) * 2015-03-12 2016-12-13 The Boeing Company Wireless data concentrators for aircraft data networks
EP3163676B1 (en) 2015-10-29 2019-04-24 Thomson Licensing Circuit board for an antenna assembly
US10181653B2 (en) 2016-07-21 2019-01-15 Infineon Technologies Ag Radio frequency system for wearable device
US10218407B2 (en) 2016-08-08 2019-02-26 Infineon Technologies Ag Radio frequency system and method for wearable device
US10466772B2 (en) 2017-01-09 2019-11-05 Infineon Technologies Ag System and method of gesture detection for a remote device
US10505255B2 (en) 2017-01-30 2019-12-10 Infineon Technologies Ag Radio frequency device packages and methods of formation thereof
US10602548B2 (en) 2017-06-22 2020-03-24 Infineon Technologies Ag System and method for gesture sensing
US10746625B2 (en) 2017-12-22 2020-08-18 Infineon Technologies Ag System and method of monitoring a structural object using a millimeter-wave radar sensor
US11346936B2 (en) 2018-01-16 2022-05-31 Infineon Technologies Ag System and method for vital signal sensing using a millimeter-wave radar sensor
US11278241B2 (en) 2018-01-16 2022-03-22 Infineon Technologies Ag System and method for vital signal sensing using a millimeter-wave radar sensor
US10795012B2 (en) 2018-01-22 2020-10-06 Infineon Technologies Ag System and method for human behavior modelling and power control using a millimeter-wave radar sensor
US10576328B2 (en) 2018-02-06 2020-03-03 Infineon Technologies Ag System and method for contactless sensing on a treadmill
US10705198B2 (en) 2018-03-27 2020-07-07 Infineon Technologies Ag System and method of monitoring an air flow using a millimeter-wave radar sensor
US10761187B2 (en) 2018-04-11 2020-09-01 Infineon Technologies Ag Liquid detection using millimeter-wave radar sensor
US10775482B2 (en) 2018-04-11 2020-09-15 Infineon Technologies Ag Human detection and identification in a setting using millimeter-wave radar
US10794841B2 (en) 2018-05-07 2020-10-06 Infineon Technologies Ag Composite material structure monitoring system
US10399393B1 (en) 2018-05-29 2019-09-03 Infineon Technologies Ag Radar sensor system for tire monitoring
US10903567B2 (en) 2018-06-04 2021-01-26 Infineon Technologies Ag Calibrating a phased array system
US11416077B2 (en) 2018-07-19 2022-08-16 Infineon Technologies Ag Gesture detection system and method using a radar sensor
US10928501B2 (en) 2018-08-28 2021-02-23 Infineon Technologies Ag Target detection in rainfall and snowfall conditions using mmWave radar
US11183772B2 (en) 2018-09-13 2021-11-23 Infineon Technologies Ag Embedded downlight and radar system
US11125869B2 (en) 2018-10-16 2021-09-21 Infineon Technologies Ag Estimating angle of human target using mmWave radar
US11397239B2 (en) 2018-10-24 2022-07-26 Infineon Technologies Ag Radar sensor FSM low power mode
US11360185B2 (en) 2018-10-24 2022-06-14 Infineon Technologies Ag Phase coded FMCW radar
EP3654053A1 (en) 2018-11-14 2020-05-20 Infineon Technologies AG Package with acoustic sensing device(s) and millimeter wave sensing elements
US11087115B2 (en) 2019-01-22 2021-08-10 Infineon Technologies Ag User authentication using mm-Wave sensor for automotive radar systems
US11355838B2 (en) 2019-03-18 2022-06-07 Infineon Technologies Ag Integration of EBG structures (single layer/multi-layer) for isolation enhancement in multilayer embedded packaging technology at mmWave
US11126885B2 (en) 2019-03-21 2021-09-21 Infineon Technologies Ag Character recognition in air-writing based on network of radars
US11454696B2 (en) 2019-04-05 2022-09-27 Infineon Technologies Ag FMCW radar integration with communication system
US11327167B2 (en) 2019-09-13 2022-05-10 Infineon Technologies Ag Human target tracking system and method
US11774592B2 (en) 2019-09-18 2023-10-03 Infineon Technologies Ag Multimode communication and radar system resource allocation
US11435443B2 (en) 2019-10-22 2022-09-06 Infineon Technologies Ag Integration of tracking with classifier in mmwave radar
US11808883B2 (en) 2020-01-31 2023-11-07 Infineon Technologies Ag Synchronization of multiple mmWave devices
US11614516B2 (en) 2020-02-19 2023-03-28 Infineon Technologies Ag Radar vital signal tracking using a Kalman filter
US11585891B2 (en) 2020-04-20 2023-02-21 Infineon Technologies Ag Radar-based vital sign estimation
US11567185B2 (en) 2020-05-05 2023-01-31 Infineon Technologies Ag Radar-based target tracking using motion detection
US11774553B2 (en) 2020-06-18 2023-10-03 Infineon Technologies Ag Parametric CNN for radar processing
US11704917B2 (en) 2020-07-09 2023-07-18 Infineon Technologies Ag Multi-sensor analysis of food
US11614511B2 (en) 2020-09-17 2023-03-28 Infineon Technologies Ag Radar interference mitigation
US11719787B2 (en) 2020-10-30 2023-08-08 Infineon Technologies Ag Radar-based target set generation
US11719805B2 (en) 2020-11-18 2023-08-08 Infineon Technologies Ag Radar based tracker using empirical mode decomposition (EMD) and invariant feature transform (IFT)
US11662430B2 (en) 2021-03-17 2023-05-30 Infineon Technologies Ag MmWave radar testing

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4739448A (en) * 1984-06-25 1988-04-19 Magnavox Government And Industrial Electronics Company Microwave multiport multilayered integrated circuit chip carrier
US6418031B1 (en) * 2000-05-01 2002-07-09 International Business Machines Corporation Method and means for decoupling a printed circuit board
US6900992B2 (en) * 2001-09-18 2005-05-31 Intel Corporation Printed circuit board routing and power delivery for high frequency integrated circuits
US20050225955A1 (en) * 2004-04-09 2005-10-13 Hewlett-Packard Development Company, L.P. Multi-layer printed circuit boards

Family Cites Families (332)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3585537A (en) 1969-02-10 1971-06-15 Bell Telephone Labor Inc Electric wave filters
US3596228A (en) 1969-05-29 1971-07-27 Ibm Fluid actuated contactor
US3727710A (en) * 1971-05-13 1973-04-17 Gen Motors Corp Steer control for a track-laying vehicle
US3899028A (en) 1972-03-30 1975-08-12 Systron Donner Corp Angular position sensing and control system, apparatus and method
US3815272A (en) 1973-01-03 1974-06-11 G Marleau Collapsible, triangular net assembly
FR2280985B1 (en) 1974-08-01 1977-01-07 Lignes Telegraph Telephon WIDE BAND MINIATURIZED ANTENNA
US4637474A (en) * 1974-11-05 1987-01-20 Leonard Willie B Tractor and towed implement with elevation control system for implement including pressure responsive valve actuator
US4132272A (en) * 1977-06-30 1979-01-02 International Harvester Company Tractor hitch position control system
US4170776A (en) 1977-12-21 1979-10-09 Nasa System for near real-time crustal deformation monitoring
US4180133A (en) 1978-01-12 1979-12-25 Iowa State University Research Foundation, Inc. Guidance system for towed vehicles
DE2942557C2 (en) 1979-10-22 1983-01-27 Siemens AG, 1000 Berlin und 8000 München Directional antenna arrangement or directional antenna for a jammer
JPS639141Y2 (en) 1980-10-22 1988-03-18
US4769700A (en) 1981-11-20 1988-09-06 Diffracto Ltd. Robot tractors
US4894662A (en) * 1982-03-01 1990-01-16 Western Atlas International, Inc. Method and system for determining position on a moving platform, such as a ship, using signals from GPS satellites
US4667203A (en) 1982-03-01 1987-05-19 Aero Service Div, Western Geophysical Method and system for determining position using signals from satellites
US4453614A (en) 1982-03-19 1984-06-12 Deere & Company Steering arrangement for an off-highway articulated vehicle
US4689556A (en) 1984-10-12 1987-08-25 Daymarc Corporation Broad band contactor assembly for testing integrated circuit devices
US4785463A (en) 1985-09-03 1988-11-15 Motorola, Inc. Digital global positioning system receiver
US4710775A (en) 1985-09-30 1987-12-01 The Boeing Company Parasitically coupled, complementary slot-dipole antenna element
US4714435A (en) 1985-11-14 1987-12-22 Molex Incorporated Connection for flexible apparatus
US4751512A (en) 1986-01-21 1988-06-14 Oceanonics, Inc. Differential navigation system for remote mobile users
US4694264A (en) 1986-03-05 1987-09-15 The United States Of America As Represented By The United States Department Of Energy Radio frequency coaxial feedthrough device
US4812991A (en) * 1986-05-01 1989-03-14 Magnavox Govt. And Industrial Electronics Company Method for precision dynamic differential positioning
US4802545A (en) * 1986-10-15 1989-02-07 J. I. Case Company Steering control system for articulated vehicle
US4858132A (en) 1987-09-11 1989-08-15 Ndc Technologies, Inc. Optical navigation system for an automatic guided vehicle, and method
US4864320A (en) 1988-05-06 1989-09-05 Ball Corporation Monopole/L-shaped parasitic elements for circularly/elliptically polarized wave transceiving
US5031704A (en) 1988-05-10 1991-07-16 Fleischer Manufacturing, Inc. Guidance control apparatus for agricultural implement
US4813991A (en) * 1988-05-20 1989-03-21 Thomson Consumer Electronics, Inc. Universal stem mold for manufacturing a molded glass stem
US4918607A (en) * 1988-09-09 1990-04-17 Caterpillar Industrial Inc. Vehicle guidance system
US4916577A (en) * 1988-12-20 1990-04-10 Grumman Aerospace Corporation Method of mounting removable modules
US5165109A (en) 1989-01-19 1992-11-17 Trimble Navigation Microwave communication antenna
US5177489A (en) * 1989-09-26 1993-01-05 Magnavox Electronic Systems Company Pseudolite-aided method for precision kinematic positioning
US4963889A (en) 1989-09-26 1990-10-16 Magnavox Government And Industrial Electronics Company Method and apparatus for precision attitude determination and kinematic positioning
US5173715A (en) 1989-12-04 1992-12-22 Trimble Navigation Antenna with curved dipole elements
US5191351A (en) * 1989-12-29 1993-03-02 Texas Instruments Incorporated Folded broadband antenna with a symmetrical pattern
US5375059A (en) 1990-02-05 1994-12-20 Caterpillar Inc. Vehicle position determination system and method
US5680306A (en) 1990-02-05 1997-10-21 Caterpillar Inc. System, and method for enabling a vehicle to track a path
US5156219A (en) 1990-06-04 1992-10-20 A.I.L., Inc. Positioning apparatus for drawn implement
US5100229A (en) * 1990-08-17 1992-03-31 Spatial Positioning Systems, Inc. Spatial positioning system
US5185610A (en) * 1990-08-20 1993-02-09 Texas Instruments Incorporated GPS system and method for deriving pointing or attitude from a single GPS receiver
US5155493A (en) 1990-08-28 1992-10-13 The United States Of America As Represented By The Secretary Of The Air Force Tape type microstrip patch antenna
US5155490A (en) 1990-10-15 1992-10-13 Gps Technology Corp. Geodetic surveying system using multiple GPS base stations
US5390207A (en) * 1990-11-28 1995-02-14 Novatel Communications Ltd. Pseudorandom noise ranging receiver which compensates for multipath distortion by dynamically adjusting the time delay spacing between early and late correlators
US5294970A (en) * 1990-12-31 1994-03-15 Spatial Positioning Systems, Inc. Spatial positioning system
US5152347A (en) 1991-04-05 1992-10-06 Deere & Company Interface system for a towed implement
US5134407A (en) * 1991-04-10 1992-07-28 Ashtech Telesis, Inc. Global positioning system receiver digital processing technique
US5202829A (en) * 1991-06-10 1993-04-13 Trimble Navigation Limited Exploration system and method for high-accuracy and high-confidence level relative position and velocity determinations
US5148179A (en) 1991-06-27 1992-09-15 Trimble Navigation Differential position determination using satellites
WO1993002905A1 (en) 1991-07-30 1993-02-18 Aura Systems, Inc. Variable gain servo assist
US5365447A (en) 1991-09-20 1994-11-15 Dennis Arthur R GPS and satelite navigation system
US5239669A (en) 1992-02-04 1993-08-24 Trimble Navigation Limited Coupler for eliminating a hardwire connection between a handheld global positioning system (GPS) receiver and a stationary remote antenna
US5323322A (en) 1992-03-05 1994-06-21 Trimble Navigation Limited Networked differential GPS system
US5255756A (en) 1992-04-22 1993-10-26 Progressive Farm Products, Inc. Caddy with guidance system for agricultural implements
US5343209A (en) 1992-05-07 1994-08-30 Sennott James W Navigation receiver with coupled signal-tracking channels
US5919242A (en) 1992-05-14 1999-07-06 Agri-Line Innovations, Inc. Method and apparatus for prescription application of products to an agricultural field
JP2904241B2 (en) 1992-07-01 1999-06-14 ケイディディ株式会社 Transmission method of differential data signal
US5268695A (en) 1992-10-06 1993-12-07 Trimble Navigation Limited Differential phase measurement through antenna multiplexing
US5361212A (en) 1992-11-02 1994-11-01 Honeywell Inc. Differential GPS landing assistance system
US5296861A (en) * 1992-11-13 1994-03-22 Trimble Navigation Limited Method and apparatus for maximum likelihood estimation direct integer search in differential carrier phase attitude determination systems
US5390124A (en) * 1992-12-01 1995-02-14 Caterpillar Inc. Method and apparatus for improving the accuracy of position estimates in a satellite based navigation system
US5359332A (en) 1992-12-31 1994-10-25 Trimble Navigation Limited Determination of phase ambiguities in satellite ranges
US5523761A (en) 1993-01-12 1996-06-04 Trimble Navigation Limited Differential GPS smart antenna device
US5471217A (en) 1993-02-01 1995-11-28 Magnavox Electronic Systems Company Method and apparatus for smoothing code measurements in a global positioning system receiver
US5444453A (en) 1993-02-02 1995-08-22 Ball Corporation Microstrip antenna structure having an air gap and method of constructing same
US5739785A (en) * 1993-03-04 1998-04-14 Trimble Navigation Limited Location and generation of high accuracy survey control marks using satellites
US5311149A (en) 1993-03-12 1994-05-10 Trimble Navigation Limited Integrated phase locked loop local oscillator
US5392863A (en) 1993-03-19 1995-02-28 Richard Fixemer Guidance system for an agricultural implement
US5548293A (en) 1993-03-24 1996-08-20 Leland Stanford Junior University System and method for generating attitude determinations using GPS
US5583513A (en) 1993-03-24 1996-12-10 Board Of Trustees Of The Leland Stanford Junior University System and method for generating precise code based and carrier phase position determinations
US5334987A (en) 1993-04-01 1994-08-02 Spectra-Physics Laserplane, Inc. Agricultural aircraft control system using the global positioning system
US5490073A (en) * 1993-04-05 1996-02-06 Caterpillar Inc. Differential system and method for a satellite based navigation
US5477228A (en) 1993-04-13 1995-12-19 Differential Corrections Inc. Differential global positioning system using radio data system
US5416712A (en) 1993-05-28 1995-05-16 Trimble Navigation Limited Position and velocity estimation system for adaptive weighting of GPS and dead-reckoning information
US6542077B2 (en) * 1993-06-08 2003-04-01 Raymond Anthony Joao Monitoring apparatus for a vehicle and/or a premises
US5504482A (en) * 1993-06-11 1996-04-02 Rockwell International Corporation Automobile navigation guidance, control and safety system
US5534875A (en) 1993-06-18 1996-07-09 Adroit Systems, Inc. Attitude determining system for use with global positioning system
EP0642108B1 (en) 1993-08-07 2002-03-06 Aisin Aw Co., Ltd. Navigation system
US5369589A (en) 1993-09-15 1994-11-29 Trimble Navigation Limited Plural information display for navigation
US5521610A (en) 1993-09-17 1996-05-28 Trimble Navigation Limited Curved dipole antenna with center-post amplifier
FR2710780B1 (en) * 1993-09-30 1995-10-27 Commissariat Energie Atomique Open magnetic structures.
WO1995018432A1 (en) 1993-12-30 1995-07-06 Concord, Inc. Field navigation system
US5477458A (en) 1994-01-03 1995-12-19 Trimble Navigation Limited Network for carrier phase differential GPS corrections
US5546093A (en) 1994-01-04 1996-08-13 Caterpillar Inc. System and method for providing navigation signals to an earthmoving or construction machine
US5568152A (en) 1994-02-04 1996-10-22 Trimble Navigation Limited Integrated image transfer for remote target location
JPH07230315A (en) 1994-02-16 1995-08-29 Fuji Heavy Ind Ltd Traveling controller for autonomously traveling vehicle
US5519620A (en) 1994-02-18 1996-05-21 Trimble Navigation Limited Centimeter accurate global positioning system receiver for on-the-fly real-time kinematic measurement and control
US5617100A (en) * 1994-04-07 1997-04-01 Matsushita Electric Industrial Co., Ltd. Accurate position measuring system
US5491636A (en) * 1994-04-19 1996-02-13 Glen E. Robertson Anchorless boat positioning employing global positioning system
FI942218A0 (en) 1994-05-13 1994-05-13 Modulaire Oy Automatic storage system Foer obemannat fordon
US5495257A (en) * 1994-07-19 1996-02-27 Trimble Navigation Limited Inverse differential corrections for SATPS mobile stations
US5680140A (en) 1994-07-19 1997-10-21 Trimble Navigation Limited Post-processing of inverse differential corrections for SATPS mobile stations
US5451964A (en) 1994-07-29 1995-09-19 Del Norte Technology, Inc. Method and system for resolving double difference GPS carrier phase integer ambiguity utilizing decentralized Kalman filters
US5442363A (en) 1994-08-04 1995-08-15 U.S. Army Corps Of Engineers As Represented By The Secretary Of The Army Kinematic global positioning system of an on-the-fly apparatus for centimeter-level positioning for static or moving applications
US5568162A (en) 1994-08-08 1996-10-22 Trimble Navigation Limited GPS navigation and differential-correction beacon antenna combination
US5596328A (en) * 1994-08-23 1997-01-21 Honeywell Inc. Fail-safe/fail-operational differential GPS ground station system
EP0776484B1 (en) * 1994-08-23 1998-09-30 Honeywell Inc. Differential gps ground station system
US5610845A (en) * 1994-08-30 1997-03-11 United Technologies Corporation Multi-parameter air data sensing technique
US6061390A (en) 1994-09-02 2000-05-09 California Institute Of Technology P-code enhanced method for processing encrypted GPS signals without knowledge of the encryption code
US5511623A (en) * 1994-09-12 1996-04-30 Orthman Manufacturing, Inc. Quick hitch guidance device
US5543804A (en) 1994-09-13 1996-08-06 Litton Systems, Inc. Navagation apparatus with improved attitude determination
US5604506A (en) * 1994-12-13 1997-02-18 Trimble Navigation Limited Dual frequency vertical antenna
US5589835A (en) 1994-12-20 1996-12-31 Trimble Navigation Limited Differential GPS receiver system linked by infrared signals
US5600670A (en) * 1994-12-21 1997-02-04 Trimble Navigation, Ltd. Dynamic channel allocation for GPS receivers
US5731786A (en) * 1994-12-29 1998-03-24 Trimble Navigation Limited Compaction of SATPS information for subsequent signal processing
WO1996022546A1 (en) * 1995-01-17 1996-07-25 The Board Of Trustees Of The Leland Stanford Junior University Wide area differential gps reference system and method
US5617317A (en) * 1995-01-24 1997-04-01 Honeywell Inc. True north heading estimator utilizing GPS output information and inertial sensor system output information
US5854987A (en) 1995-02-22 1998-12-29 Honda Giken Kogyo Kabushiki Kaisha Vehicle steering control system using navigation system
US5578813A (en) 1995-03-02 1996-11-26 Allen; Ross R. Freehand image scanning device which compensates for non-linear movement
US5608393A (en) * 1995-03-07 1997-03-04 Honeywell Inc. Differential ground station repeater
US5592382A (en) * 1995-03-10 1997-01-07 Rockwell International Corporation Directional steering and navigation indicator
US5646857A (en) * 1995-03-31 1997-07-08 Trimble Navigation Limited Use of an altitude sensor to augment availability of GPS location fixes
DE59501555D1 (en) * 1995-04-20 1998-04-09 Fuba Automotive Gmbh Flat antenna arrangement
US5638077A (en) 1995-05-04 1997-06-10 Rockwell International Corporation Differential GPS for fleet base stations with vector processing mechanization
US5561432A (en) 1995-05-12 1996-10-01 Trimble Navigation Out of plane antenna vector system and method
US6236907B1 (en) 1995-05-30 2001-05-22 Ag-Chem Equipment Co., Inc. System and method for creating agricultural decision and application maps for automated agricultural machines
US5875408A (en) * 1995-07-17 1999-02-23 Imra America, Inc. Automated vehicle guidance system and method for automatically guiding a vehicle
US5953367A (en) 1995-08-09 1999-09-14 Magellan Corporation Spread spectrum receiver using a pseudo-random noise code for ranging applications in a way that reduces errors when a multipath signal is present
US5862501A (en) * 1995-08-18 1999-01-19 Trimble Navigation Limited Guidance control system for movable machinery
ES2131959T3 (en) * 1995-09-01 1999-08-01 Konle Tilmar SYSTEM TO DETERMINE THE POSITION OF MOBILE OBJECTS.
US5717593A (en) * 1995-09-01 1998-02-10 Gvili; Michael E. Lane guidance system
DE19536601A1 (en) * 1995-09-19 1997-03-20 Teldix Gmbh Navigation system for a vehicle, in particular for a land vehicle
US5673491A (en) 1995-10-20 1997-10-07 Brenna; Douglas J. Crane level indicator device
JP3171119B2 (en) 1995-12-04 2001-05-28 トヨタ自動車株式会社 Automatic driving control device for vehicles
US5812961A (en) 1995-12-28 1998-09-22 Trimble Navigation Limited Method and reciever using a low earth orbiting satellite signal to augment the global positioning system
US5928309A (en) 1996-02-05 1999-07-27 Korver; Kelvin Navigation/guidance system for a land-based vehicle
SE519541C2 (en) * 1996-10-02 2003-03-11 Ericsson Telefon Ab L M Method and apparatus for transforming a real digital broadband bandpass signal into a set of digital baseband signals with I and Q components
US6014101A (en) * 1996-02-26 2000-01-11 Trimble Navigation Limited Post-processing of inverse DGPS corrections
US5828336A (en) 1996-03-29 1998-10-27 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Robust real-time wide-area differential GPS navigation
US5864318A (en) * 1996-04-26 1999-01-26 Dorne & Margolin, Inc. Composite antenna for cellular and gps communications
FR2748571B1 (en) 1996-05-09 1998-08-07 Europ Agence Spatiale RECEIVER DEVICE FOR A NAVIGATION SYSTEM IN PARTICULAR BY SATELLITE
US5935183A (en) 1996-05-20 1999-08-10 Caterpillar Inc. Method and system for determining the relationship between a laser plane and an external coordinate system
US5948044A (en) 1996-05-20 1999-09-07 Harris Corporation Hybrid GPS/inertially aided platform stabilization system
US5725230A (en) * 1996-06-17 1998-03-10 Walkup; Joseph L. Self steering tandem hitch
DE19624719A1 (en) 1996-06-21 1998-01-02 Claas Ohg System for determining the position of mobile objects, in particular vehicles
US6057800A (en) 1996-06-28 2000-05-02 State University Of New York RDOP surface for GPS relative positioning
DE19629618A1 (en) 1996-07-23 1998-01-29 Claas Ohg Route planning system for agricultural work vehicles
US5810095A (en) 1996-07-25 1998-09-22 Case Corporation System for controlling the position of an implement attached to a work vehicle
AUPO135296A0 (en) 1996-08-01 1996-08-22 Great Western Corporation Pty Ltd Agricultural cultivator
US5929721A (en) 1996-08-06 1999-07-27 Motorola Inc. Ceramic filter with integrated harmonic response suppression using orthogonally oriented low-pass filter
KR0183299B1 (en) * 1996-11-04 1999-04-15 삼성전자주식회사 Navigation apparatus notifying surrounding situation of vehicle and control method thereof
US5926079A (en) 1996-12-05 1999-07-20 Motorola Inc. Ceramic waveguide filter with extracted pole
US5757316A (en) 1997-02-01 1998-05-26 Litton Systems, Inc. Attitude determination utilizing an inertial measurement unit and a plurality of satellite transmitters
US5777578A (en) 1997-02-10 1998-07-07 National Science Council Global positioning system (GPS) Compass
US5877725A (en) * 1997-03-06 1999-03-02 Trimble Navigation Limited Wide augmentation system retrofit receiver
US5864315A (en) * 1997-04-07 1999-01-26 General Electric Company Very low power high accuracy time and frequency circuits in GPS based tracking units
US5914685A (en) 1997-04-25 1999-06-22 Magellan Corporation Relative position measuring techniques using both GPS and GLONASS carrier phase measurements
US5987383C1 (en) 1997-04-28 2006-06-13 Trimble Navigation Ltd Form line following guidance system
US6052647A (en) * 1997-06-20 2000-04-18 Stanford University Method and system for automatic control of vehicles based on carrier phase differential GPS
US5912798A (en) 1997-07-02 1999-06-15 Landsten Chu Dielectric ceramic filter
US5936573A (en) 1997-07-07 1999-08-10 Trimble Navigation Limited Real-time kinematic integrity estimator and monitor
US5940026A (en) 1997-07-21 1999-08-17 Rockwell Science Center, Inc. Azimuth determination for GPS/INS systems via GPS null steering antenna
US5917448A (en) 1997-08-07 1999-06-29 Rockwell Science Center, Inc. Attitude determination system with sequencing antenna inputs
US6061632A (en) 1997-08-18 2000-05-09 Trimble Navigation Limited Receiver with seamless correction capacity
US5943008A (en) 1997-09-23 1999-08-24 Rockwell Science Center, Inc. Single global positioning system receiver capable of attitude determination
US5927603A (en) 1997-09-30 1999-07-27 J. R. Simplot Company Closed loop control system, sensing apparatus and fluid application system for a precision irrigation device
US6023239A (en) * 1997-10-08 2000-02-08 Arinc, Inc. Method and system for a differential global navigation satellite system aircraft landing ground station
US6198992B1 (en) * 1997-10-10 2001-03-06 Trimble Navigation Limited Override for guidance control system
US6233511B1 (en) 1997-11-26 2001-05-15 Case Corporation Electronic control for a two-axis work implement
US5918558A (en) 1997-12-01 1999-07-06 Case Corporation Dual-pump, flow-isolated hydraulic circuit for an agricultural tractor
US5949374A (en) * 1997-12-15 1999-09-07 Trimble Navigation Limited Two-channel fast-sequencing high-dynamics GPS navigation receiver
US5945917A (en) 1997-12-18 1999-08-31 Rockwell International Swathing guidance display
US5969670A (en) 1998-01-22 1999-10-19 Trimble Navigation Limited Inexpensive monitoring technique for achieving high level integrity monitoring for differential GPS
US6314348B1 (en) 1998-02-11 2001-11-06 Trimble Navigation Limited Correction control for guidance control system
US6100842A (en) 1998-02-20 2000-08-08 Trimble Navigation Limited Chained location determination system
US6081171A (en) 1998-04-08 2000-06-27 Nokia Mobile Phones Limited Monolithic filters utilizing thin film bulk acoustic wave devices and minimum passive components for controlling the shape and width of a passband response
US6144335A (en) 1998-04-14 2000-11-07 Trimble Navigation Limited Automated differential correction processing of field data in a global positional system
US6356602B1 (en) * 1998-05-04 2002-03-12 Trimble Navigation Limited RF integrated circuit for downconverting a GPS signal
AUPP375498A0 (en) 1998-05-29 1998-06-18 Small, David A method for creating a network positioning system (NPS)
DE19830858A1 (en) * 1998-07-10 2000-01-13 Claas Selbstfahr Erntemasch Device and method for determining a virtual position
US5933110A (en) 1998-07-13 1999-08-03 Arinc, Inc. Vessel attitude determination system and method
US6199000B1 (en) * 1998-07-15 2001-03-06 Trimble Navigation Limited Methods and apparatus for precision agriculture operations utilizing real time kinematic global positioning system systems
US6307505B1 (en) 1998-07-22 2001-10-23 Trimble Navigation Limited Apparatus and method for coupling data to a position determination device
US5949371A (en) 1998-07-27 1999-09-07 Trimble Navigation Limited Laser based reflectors for GPS positioning augmentation
US6515619B1 (en) * 1998-07-30 2003-02-04 Mckay, Jr. Nicholas D. Object location system
US6313788B1 (en) 1998-08-14 2001-11-06 Seagull Technology, Inc. Method and apparatus for reliable inter-antenna baseline determination
US6501422B1 (en) 1998-08-19 2002-12-31 Trimble Navigation, Ltd. Precise parallel swathing guidance via satellite navigation and tilt measurement
US6230097B1 (en) 1998-08-31 2001-05-08 Trimble Navigation Limited Accurate vehicle navigation
US6256583B1 (en) 1998-09-16 2001-07-03 Rockwell Collins, Inc. GPS attitude determination system and method using optimal search space identification for integer cycle ambiguity resolution
FR2783945B1 (en) * 1998-09-29 2000-12-15 Pellenc Sa PROCESS FOR EXPLOITING LOCALIZED AGRICULTURAL DATA TO OPTIMIZE THE CULTIVATION OF PERENNIAL PLANTS
US6253160B1 (en) 1999-01-15 2001-06-26 Trimble Navigation Ltd. Method and apparatus for calibrating a tool positioning mechanism on a mobile machine
US6198430B1 (en) * 1999-03-26 2001-03-06 Rockwell Collins, Inc. Enhanced differential GNSS carrier-smoothed code processing using dual frequency measurements
US6236916B1 (en) 1999-03-29 2001-05-22 Caterpillar Inc. Autoguidance system and method for an agricultural machine
US6453237B1 (en) 1999-04-23 2002-09-17 Global Locate, Inc. Method and apparatus for locating and providing services to mobile devices
DE19919321A1 (en) 1999-04-28 2000-11-02 Deere & Co Steering system and harvesting machine
US6191733B1 (en) * 1999-06-01 2001-02-20 Modular Mining Systems, Inc. Two-antenna positioning system for surface-mine equipment
US6325684B1 (en) 1999-06-11 2001-12-04 Johnson Outdoors, Inc., Trolling motor steering control
US6236924B1 (en) 1999-06-21 2001-05-22 Caterpillar Inc. System and method for planning the operations of an agricultural machine in a field
US6275758B1 (en) 1999-06-29 2001-08-14 Caterpillar Inc. Method and apparatus for determining a cross slope of a surface
US6266595B1 (en) 1999-08-12 2001-07-24 Martin W. Greatline Method and apparatus for prescription application of products to an agricultural field
US6292132B1 (en) 1999-08-13 2001-09-18 Daimlerchrysler Ag System and method for improved accuracy in locating and maintaining positions using GPS
US6076612A (en) 1999-08-31 2000-06-20 Case Corporation Transition from position to draft mode controlled by hitch position command and feedback
US6285320B1 (en) 1999-09-03 2001-09-04 Sikorsky Aircraft Corporation Apparatus and method for mapping surfaces of an object
US6062317A (en) 1999-09-03 2000-05-16 Caterpillar Inc. Method and apparatus for controlling the direction of travel of an earthworking machine
IL132191A (en) 1999-10-03 2008-04-13 Azimuth Technologies Ltd Method for calibrating and verifying the attitude of a compass
US6611755B1 (en) 1999-12-19 2003-08-26 Trimble Navigation Ltd. Vehicle tracking, communication and fleet management system
ATE276564T1 (en) 2000-03-14 2004-10-15 Siemens Ag ROUTE PLANNING SYSTEM
US6469663B1 (en) 2000-03-21 2002-10-22 Csi Wireless Inc. Method and system for GPS and WAAS carrier phase measurements for relative positioning
GB0011493D0 (en) 2000-05-13 2000-06-28 Koninkl Philips Electronics Nv Method and apparatus for code phase tracking
US6819269B2 (en) 2000-05-17 2004-11-16 Omega Patents, L.L.C. Vehicle tracker including battery monitoring feature and related methods
US6421003B1 (en) 2000-05-19 2002-07-16 Sri International Attitude determination using multiple baselines in a navigational positioning system
US6259398B1 (en) 2000-05-19 2001-07-10 Sri International Multi-valued variable ambiguity resolution for satellite navigation signal carrier wave path length determination
GB2368218B (en) 2000-06-01 2004-04-28 Furuno Electric Co System for determining the heading and/or attitude of a body
AU2001268181A1 (en) 2000-06-05 2001-12-17 Ag-Chem Equipment Company, Inc. System and method for creating demo application maps for site-specific farming
US6397147B1 (en) 2000-06-06 2002-05-28 Csi Wireless Inc. Relative GPS positioning using a single GPS receiver with internally generated differential correction terms
GB0014719D0 (en) 2000-06-16 2000-08-09 Koninkl Philips Electronics Nv A method of providing an estimate of a location
US6445983B1 (en) 2000-07-07 2002-09-03 Case Corporation Sensor-fusion navigator for automated guidance of off-road vehicles
JP4446569B2 (en) 2000-07-24 2010-04-07 古野電気株式会社 Carrier phase relative positioning device
US6631916B1 (en) 2000-07-28 2003-10-14 Merle E. Miller Guidance system for pull-type equipment
US6931233B1 (en) 2000-08-31 2005-08-16 Sirf Technology, Inc. GPS RF front end IC with programmable frequency synthesizer for use in wireless phones
JP3721973B2 (en) * 2000-09-28 2005-11-30 日産自動車株式会社 Vehicle steering device
US6377889B1 (en) * 2000-10-13 2002-04-23 Trimble Navigation Limited Non-linear method of guiding to arbitrary curves with adaptive feedback
US6380888B1 (en) * 2000-11-13 2002-04-30 The United States Of America As Represented By The Secretary Of The Navy Self-contained, self-surveying differential GPS base station and method of operating same
US6643576B1 (en) 2000-11-15 2003-11-04 Integrinautics Corporation Rapid adjustment of trajectories for land vehicles
US6711501B2 (en) * 2000-12-08 2004-03-23 Satloc, Llc Vehicle navigation system and method for swathing applications
US6553311B2 (en) * 2000-12-08 2003-04-22 Trimble Navigation Limited Navigational off- line and off-heading indication system and method
US6539303B2 (en) * 2000-12-08 2003-03-25 Mcclure John A. GPS derived swathing guidance system
US6577952B2 (en) 2001-01-08 2003-06-10 Motorola, Inc. Position and heading error-correction method and apparatus for vehicle navigation systems
EP1358503A4 (en) 2001-02-05 2004-05-26 Clark Cohen Low cost system and method for making dual band gps measurements
US6754584B2 (en) 2001-02-28 2004-06-22 Enpoint, Llc Attitude measurement using a single GPS receiver with two closely-spaced antennas
US6445990B1 (en) 2001-03-19 2002-09-03 Caterpillar Inc. Method and apparatus for controlling straight line travel of a tracked machine
DE10114091A1 (en) * 2001-03-22 2002-09-26 Deere & Co Control device for a vehicle mounting interface
GB2379112B (en) 2001-03-28 2003-10-15 Comm Res Lab Method for acquiring azimuth information
JP2002311123A (en) * 2001-04-11 2002-10-23 Mitsui & Co Ltd Satellite position measuring system
US6732024B2 (en) 2001-05-07 2004-05-04 The Board Of Trustees Of The Leland Stanford Junior University Method and apparatus for vehicle control, navigation and positioning
US6721638B2 (en) 2001-05-07 2004-04-13 Rapistan Systems Advertising Corp. AGV position and heading controller
US6622091B2 (en) 2001-05-11 2003-09-16 Fibersense Technology Corporation Method and system for calibrating an IG/GP navigational system
US6434462B1 (en) 2001-06-28 2002-08-13 Deere & Company GPS control of a tractor-towed implement
US6516271B2 (en) * 2001-06-29 2003-02-04 The Regents Of The University Of California Method and apparatus for ultra precise GPS-based mapping of seeds or vegetation during planting
US6553300B2 (en) * 2001-07-16 2003-04-22 Deere & Company Harvester with intelligent hybrid control system
US6587761B2 (en) 2001-10-23 2003-07-01 The Aerospace Corporation Unambiguous integer cycle attitude determination method
US6985811B2 (en) 2001-10-30 2006-01-10 Sirf Technology, Inc. Method and apparatus for real time clock (RTC) brownout detection
JP4116792B2 (en) 2001-12-19 2008-07-09 古野電気株式会社 Carrier phase relative positioning device
US6671587B2 (en) 2002-02-05 2003-12-30 Ford Motor Company Vehicle dynamics measuring apparatus and method using multiple GPS antennas
JP2003232845A (en) 2002-02-12 2003-08-22 Furuno Electric Co Ltd Detection device of azimuth and attitude of moving body
JP4856851B2 (en) * 2002-04-05 2012-01-18 イー・アイ・デュポン・ドウ・ヌムール・アンド・カンパニー Method and apparatus for controlling an outgassing process
US6865465B2 (en) * 2002-05-06 2005-03-08 Csi Wireless, Inc. Method and system for implement steering for agricultural vehicles
DE10224939B4 (en) 2002-05-31 2009-01-08 Deere & Company, Moline Driving-axle trailer
US6822314B2 (en) 2002-06-12 2004-11-23 Intersil Americas Inc. Base for a NPN bipolar transistor
US6657875B1 (en) 2002-07-16 2003-12-02 Fairchild Semiconductor Corporation Highly efficient step-down/step-up and step-up/step-down charge pump
EP1552247A2 (en) 2002-08-13 2005-07-13 DRS Communications Company, LLC Method and system for determining absolute positions of mobile communications devices using remotely generated positioning information
US7031725B2 (en) 2002-08-13 2006-04-18 Drs Communications Company, Llc Method and system for determining relative positions of networked mobile communication devices
JP2004125580A (en) 2002-10-02 2004-04-22 Hitachi Constr Mach Co Ltd Position measuring system of working machine
DE10250694B3 (en) * 2002-10-31 2004-02-12 CNH Österreich GmbH Agricultural vehicle control method provides automatic travel and field end management by detection, storage and controlled alteration of vehicle operating parameters
KR100506058B1 (en) 2002-11-28 2005-08-05 매그나칩 반도체 유한회사 Phase Locked Loop having Voltage Controlled Oscillator dividing frequency
US7689354B2 (en) * 2003-03-20 2010-03-30 Hemisphere Gps Llc Adaptive guidance system and method
US7162348B2 (en) * 2002-12-11 2007-01-09 Hemisphere Gps Llc Articulated equipment position control system and method
US7437230B2 (en) 2003-03-20 2008-10-14 Hemisphere Gps Llc Satellite based vehicle guidance control in straight and contour modes
US7142956B2 (en) 2004-03-19 2006-11-28 Hemisphere Gps Llc Automatic steering system and method
US8138970B2 (en) 2003-03-20 2012-03-20 Hemisphere Gps Llc GNSS-based tracking of fixed or slow-moving structures
US8271194B2 (en) 2004-03-19 2012-09-18 Hemisphere Gps Llc Method and system using GNSS phase measurements for relative positioning
US20040212533A1 (en) 2003-04-23 2004-10-28 Whitehead Michael L. Method and system for satellite based phase measurements for relative positioning of fixed or slow moving points in close proximity
US7216033B2 (en) * 2003-03-31 2007-05-08 Deere & Company Path planner and method for planning a contour path of a vehicle
US7027918B2 (en) 2003-04-07 2006-04-11 Novariant, Inc. Satellite navigation system using multiple antennas
US7191061B2 (en) * 2003-04-17 2007-03-13 Battelle Energy Alliance, Llc Auto-steering apparatus and method
US7292186B2 (en) 2003-04-23 2007-11-06 Csi Wireless Inc. Method and system for synchronizing multiple tracking devices for a geo-location system
US7119716B2 (en) * 2003-05-28 2006-10-10 Legalview Assets, Limited Response systems and methods for notification systems for modifying future notifications
US6744404B1 (en) 2003-07-09 2004-06-01 Csi Wireless Inc. Unbiased code phase estimator for mitigating multipath in GPS
US8768617B2 (en) 2003-10-06 2014-07-01 Csr Technology Inc. Method and system for a data interface for aiding a satellite positioning system receiver
US7006032B2 (en) * 2004-01-15 2006-02-28 Honeywell International, Inc. Integrated traffic surveillance apparatus
EP1591847A1 (en) 2004-04-27 2005-11-02 Abb Research Ltd. Scheduling of industrial production processes
EP1756687B1 (en) 2004-05-17 2012-04-11 Hemisphere GPS Inc. Satellite based vehicle guidance control in straight and contour modes
US7248211B2 (en) 2004-07-26 2007-07-24 Navcom Technology Inc. Moving reference receiver for RTK navigation
US7315278B1 (en) 2004-07-30 2008-01-01 Novariant, Inc. Multiple frequency antenna structures and methods for receiving navigation or ranging signals
US7089099B2 (en) 2004-07-30 2006-08-08 Automotive Technologies International, Inc. Sensor assemblies
US7271766B2 (en) 2004-07-30 2007-09-18 Novariant, Inc. Satellite and local system position determination
US7395769B2 (en) 2004-10-21 2008-07-08 Jensen Layton W Individual row rate control of farm implements to adjust the volume of crop inputs across wide implements in irregularly shaped or contour areas of chemical application, planting or seeding
FR2881008B1 (en) 2005-01-20 2007-04-20 Thales Sa SATELLITE POSITIONING RECEIVER WITH IMPROVED INTEGRITY AND CONTINUITY
US20060167600A1 (en) 2005-01-27 2006-07-27 Raven Industries, Inc. Architecturally partitioned automatic steering system and method
US7451030B2 (en) 2005-02-04 2008-11-11 Novariant, Inc. System and method for interactive selection and determination of agricultural vehicle guide paths offset from each other with varying curvature along their length
ATE374447T1 (en) 2005-02-25 2007-10-15 Nemerix Sa HALF BIN LINEAR FREQUENCY DISCRIMINATOR
US7738606B2 (en) 2005-03-24 2010-06-15 Novatel Inc. System and method for making correlation measurements utilizing pulse shape measurements
US7428259B2 (en) 2005-05-06 2008-09-23 Sirf Technology Holdings, Inc. Efficient and flexible GPS receiver baseband architecture
EP1724605A1 (en) 2005-05-18 2006-11-22 Leica Geosystems AG Method of determining position for a satellite based positioning system
US7522100B2 (en) 2005-07-01 2009-04-21 Sirf Technology Holdings, Inc. Method and device for acquiring weak global navigation satellite system (GNSS) signals
US7639181B2 (en) 2005-07-01 2009-12-29 Sirf Technology Holdings, Inc. Method and device for tracking weak global navigation satellite system (GNSS) signals
US7324915B2 (en) * 2005-07-14 2008-01-29 Biosense Webster, Inc. Data transmission to a position sensor
US7571029B2 (en) 2005-10-04 2009-08-04 Gm Global Technology Operations, Inc. Method and apparatus for reporting road conditions
US7388539B2 (en) 2005-10-19 2008-06-17 Hemisphere Gps Inc. Carrier track loop for GNSS derived attitude
ATE453125T1 (en) 2005-11-03 2010-01-15 Qualcomm Inc MULTI-BAND RECEIVER FOR NAVIGATION SATELLITE SIGNALS (GNSS)
US7742518B2 (en) 2005-11-28 2010-06-22 Honeywell International Inc. Discriminator function for GPS code alignment
JP4647486B2 (en) 2005-12-27 2011-03-09 京セラ株式会社 Transceiver circuit
US7619559B2 (en) 2006-03-15 2009-11-17 The Boeing Company Method and system for all-in-view coherent GPS signal PRN codes acquisition and navigation solution determination
US7688261B2 (en) 2006-03-15 2010-03-30 The Boeing Company Global position system (GPS) user receiver and geometric surface processing for all-in-view coherent GPS signal PRN codes acquisition and navigation solution
FR2898998B1 (en) 2006-03-21 2008-07-25 Thales Sa METHOD AND DEVICE FOR FAST CORRELATION CALCULATION
US7667645B2 (en) * 2006-05-25 2010-02-23 The Boeing Company GPS gyro calibration
FI118394B (en) 2006-05-26 2007-10-31 Savcor One Oy A system and method for locating a GPS device
CN101563625A (en) * 2006-11-06 2009-10-21 电子地图有限公司 Arrangement for and method of two dimensional and three dimensional precision location and orientation determination
US7839334B2 (en) * 2006-12-29 2010-11-23 Broadcom Corporation IC with a 55-64 GHz antenna
US7796073B2 (en) 2007-01-10 2010-09-14 Panasonic Corporation Current switch circuit and D/A converter, semiconductor integrated circuit, and communication device using the same
US20080170378A1 (en) * 2007-01-17 2008-07-17 Cheng-Yi Ou-Yang Circuit structure having independent ground plane layouts implemented in circuit board
US8000381B2 (en) 2007-02-27 2011-08-16 Hemisphere Gps Llc Unbiased code phase discriminator
ES2360769B1 (en) 2007-04-30 2012-05-08 Navento Technologies, S.L PROCEDURE AND SYSTEM OF LOCALIZATION AND DEVICE PORT�? TIL LOCALIZABLE.
US8059028B2 (en) * 2008-08-14 2011-11-15 Trueposition, Inc. Hybrid GNSS and TDOA wireless location system
KR20090076171A (en) 2008-01-07 2009-07-13 삼성전자주식회사 The method for estimating position and the apparatus thereof
US20090177395A1 (en) 2008-01-07 2009-07-09 David Stelpstra Navigation device and method
JP2011515725A (en) 2008-02-05 2011-05-19 ソニー エリクソン モバイル コミュニケーションズ, エービー Communication terminal including graphical bookmark manager
US8188917B2 (en) * 2008-02-25 2012-05-29 CSR Technology Holdings Inc. System and method for operating a GPS device in a micro power mode
WO2009126587A1 (en) 2008-04-08 2009-10-15 Hemisphere Gps Llc Gnss-based mobile communication system and method
US20090259397A1 (en) 2008-04-10 2009-10-15 Richard Stanton Navigation system with touchpad remote
US8195357B2 (en) 2008-04-16 2012-06-05 GM Global Technology Operations LLC In-vehicle sensor-based calibration algorithm for yaw rate sensor calibration
US20090262974A1 (en) 2008-04-18 2009-10-22 Erik Lithopoulos System and method for obtaining georeferenced mapping data
US8725327B2 (en) 2008-04-22 2014-05-13 Exelis Inc. Navigation system and method of obtaining accurate navigational information in signal challenging environments
TWI375012B (en) 2008-04-22 2012-10-21 En Min Jow Storage device with navigation function
US8260552B2 (en) 2008-04-30 2012-09-04 Honeywell International Inc. Systems and methods for determining location information using dual filters
US20090273513A1 (en) 2008-05-01 2009-11-05 Skytraq Technology Inc. Method of dynamically optimizing the update rate of gps output data
US8634785B2 (en) 2008-05-01 2014-01-21 Qualcomm Incorporated Radio frequency (RF) signal multiplexing
US7606567B1 (en) 2008-05-01 2009-10-20 Daniel A. Katz Channel allocation for burst transmission to a diversity of satellites
WO2009140768A1 (en) 2008-05-22 2009-11-26 Novatel Inc. Gnss receiver using signals of opportunity and assistance information to reduce the time to first fix
US8244411B2 (en) 2008-05-27 2012-08-14 Baker David A Orientation-based wireless sensing apparatus
US8035559B2 (en) 2008-05-30 2011-10-11 O2 Micro, Inc Global positioning system receiver
US7671794B2 (en) 2008-06-02 2010-03-02 Enpoint, Llc Attitude estimation using intentional translation of a global navigation satellite system (GNSS) antenna
US7940210B2 (en) 2008-06-26 2011-05-10 Honeywell International Inc. Integrity of differential GPS corrections in navigation devices using military type GPS receivers
US8239133B2 (en) * 2008-07-02 2012-08-07 O2Micro, International Global positioning system and dead reckoning (GPSandDR) integrated navigation system
US8633853B2 (en) * 2008-07-31 2014-01-21 Honeywell International Inc. Method and apparatus for location detection using GPS and WiFi/WiMAX
US7859454B2 (en) * 2008-08-15 2010-12-28 Broadcom Corporation Method and system for calibrating group delay errors in a combined GPS and GLONASS receiver
TWI332454B (en) * 2008-09-10 2010-11-01 Univ Nat Chiao Tung Intelligent vehicle traffic safety supply system
US8120529B2 (en) * 2008-09-11 2012-02-21 California Institute Of Technology Method and apparatus for autonomous, in-receiver prediction of GNSS ephemerides
US8112201B2 (en) 2008-10-02 2012-02-07 Trimble Navigation Limited Automatic control of passive, towed implements
US8031111B2 (en) 2008-10-03 2011-10-04 Trimble Navigation Limited Compact transmission of GPS information using compressed measurement record format
US8860609B2 (en) 2008-10-23 2014-10-14 Texas Instruments Incorporated Loosely-coupled integration of global navigation satellite system and inertial navigation system
JP4780174B2 (en) 2008-10-24 2011-09-28 日本ビクター株式会社 Angular velocity sensor correction device, angular velocity calculation device, angular velocity sensor correction method, angular velocity calculation method
JP4709886B2 (en) 2008-10-24 2011-06-29 株式会社エヌ・ティ・ティ・ドコモ POSITIONING CONTROL DEVICE AND POSITIONING CONTROL METHOD
US7928905B2 (en) 2008-10-26 2011-04-19 Mitac International Corp. Method of using road signs to augment global positioning system (GPS) coordinate data for calculating a current position of a personal navigation device
US8836576B2 (en) 2008-10-27 2014-09-16 Mediatek Inc. Power saving method adaptable in GNSS device
US20100106414A1 (en) 2008-10-27 2010-04-29 John Whitehead Method of performing routing with artificial intelligence
US20100111372A1 (en) 2008-11-03 2010-05-06 Microsoft Corporation Determining user similarities based on location histories
KR101677756B1 (en) 2008-11-03 2016-11-18 삼성전자주식회사 Method and apparatus for setting up automatic optimized gps reception period and map contents
US7855683B2 (en) 2008-11-04 2010-12-21 At&T Intellectual Property I, L.P. Methods and apparatuses for GPS coordinates extrapolation when GPS signals are not available
US8412456B2 (en) 2008-11-06 2013-04-02 Texas Instruments Incorporated Loosely-coupled integration of global navigation satellite system and inertial navigation system: speed scale-factor and heading bias calibration
US8447517B2 (en) 2008-11-06 2013-05-21 Texas Instruments Incorporated Tightly-coupled GNSS/IMU integration filter having speed scale-factor and heading bias calibration
US8159391B2 (en) 2008-11-13 2012-04-17 Ecole Polytechnique Federale De Lausanne (Epfl) Method to secure GNSS based locations in a device having GNSS receiver
US7948434B2 (en) 2008-11-13 2011-05-24 Broadcom Corporation Method and system for maintaining a GNSS receiver in a hot-start state

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4739448A (en) * 1984-06-25 1988-04-19 Magnavox Government And Industrial Electronics Company Microwave multiport multilayered integrated circuit chip carrier
US6418031B1 (en) * 2000-05-01 2002-07-09 International Business Machines Corporation Method and means for decoupling a printed circuit board
US6900992B2 (en) * 2001-09-18 2005-05-31 Intel Corporation Printed circuit board routing and power delivery for high frequency integrated circuits
US20050225955A1 (en) * 2004-04-09 2005-10-13 Hewlett-Packard Development Company, L.P. Multi-layer printed circuit boards

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9880562B2 (en) 2003-03-20 2018-01-30 Agjunction Llc GNSS and optical guidance and machine control
US9886038B2 (en) 2003-03-20 2018-02-06 Agjunction Llc GNSS and optical guidance and machine control
USRE47101E1 (en) 2003-03-20 2018-10-30 Agjunction Llc Control for dispensing material from vehicle
US10168714B2 (en) 2003-03-20 2019-01-01 Agjunction Llc GNSS and optical guidance and machine control
USRE48527E1 (en) 2007-01-05 2021-04-20 Agjunction Llc Optical tracking vehicle control system and method
US9002566B2 (en) 2008-02-10 2015-04-07 AgJunction, LLC Visual, GNSS and gyro autosteering control
USRE47055E1 (en) 2009-01-17 2018-09-25 Agjunction Llc Raster-based contour swathing for guidance and variable-rate chemical application
USRE48509E1 (en) 2009-01-17 2021-04-13 Agjunction Llc Raster-based contour swathing for guidance and variable-rate chemical application
USRE47648E1 (en) 2009-09-17 2019-10-15 Agjunction Llc Integrated multi-sensor control system and method

Also Published As

Publication number Publication date
US20090085815A1 (en) 2009-04-02
WO2009066183A3 (en) 2011-04-28
US7948769B2 (en) 2011-05-24

Similar Documents

Publication Publication Date Title
WO2009066183A2 (en) Tightly-coupled pcb gnss circuit and manufacturing method
US6731245B1 (en) Compact conformal patch antenna
JP2004159288A (en) Antenna assembly, printed wiring board, printed board, communication adapter, and portable electronic apparatus
US8692732B2 (en) Antenna with multiple folds
JP7000964B2 (en) Multi-layer transmission line
JPH1188209A (en) Mobile communication equipment
JP6567364B2 (en) Pattern antenna
KR20140147696A (en) attenuation reduction grounding structure for differential-mode signal transmission lines of flexible circuit board
US7186924B2 (en) Dielectric structure for printed circuit board traces
KR20120051012A (en) Microwave filter
JP4968033B2 (en) Antenna device
US7394440B2 (en) Three-dimensional antenna fabrication from multiple two-dimensional structures
US20230170613A1 (en) Feed network and antenna
JP5644702B2 (en) Antenna device
CN110431714B (en) Patch antenna feed unit
KR101438188B1 (en) Improvement in the offset footprint of a connector on a printed board
US20190357349A1 (en) 3d electromagnetic bandgap circuit
JP6827190B2 (en) Antenna device
JP2017228834A (en) Distributor synthesizer, distributor, and synthesizer
JPH0766620A (en) Antenna
JP7152984B2 (en) Receiver circuit board and receiver circuit
JP2003234613A (en) Antenna element
CN102340926A (en) Printed circuit board
JP2003198232A (en) Portable communication terminal
CN212848807U (en) Dual wiring antenna structure

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 08851266

Country of ref document: EP

Kind code of ref document: A2

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 08851266

Country of ref document: EP

Kind code of ref document: A2