DE69127414D1 - Werfersteuersystem - Google Patents
WerfersteuersystemInfo
- Publication number
- DE69127414D1 DE69127414D1 DE69127414T DE69127414T DE69127414D1 DE 69127414 D1 DE69127414 D1 DE 69127414D1 DE 69127414 T DE69127414 T DE 69127414T DE 69127414 T DE69127414 T DE 69127414T DE 69127414 D1 DE69127414 D1 DE 69127414D1
- Authority
- DE
- Germany
- Prior art keywords
- control system
- launcher control
- launcher
- control
- Prior art date
- Legal status (The legal status 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 status listed.)
- Expired - Lifetime
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
- F41G7/30—Command link guidance systems
- F41G7/301—Details
- F41G7/306—Details for transmitting guidance signals
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/568,298 US5118050A (en) | 1989-12-07 | 1990-08-16 | Launcher control system |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69127414D1 true DE69127414D1 (de) | 1997-10-02 |
DE69127414T2 DE69127414T2 (de) | 1998-01-02 |
Family
ID=24270730
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69127414T Expired - Lifetime DE69127414T2 (de) | 1990-08-16 | 1991-07-25 | Werfersteuersystem |
Country Status (8)
Country | Link |
---|---|
US (1) | US5118050A (de) |
EP (1) | EP0471225B1 (de) |
JP (1) | JP2530777B2 (de) |
CA (1) | CA2046788A1 (de) |
DE (1) | DE69127414T2 (de) |
IL (1) | IL98906A0 (de) |
NO (1) | NO306313B1 (de) |
TR (1) | TR26547A (de) |
Families Citing this family (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5221062A (en) * | 1989-12-07 | 1993-06-22 | Hughes Aircraft Company | Frequency synthesizer |
US5186414A (en) * | 1992-04-20 | 1993-02-16 | The United States Of America As Represented By The Secretary Of The Navy | Hybrid data link |
US5471213A (en) * | 1994-07-26 | 1995-11-28 | Hughes Aircraft Company | Multiple remoted weapon alerting and cueing system |
US5657947A (en) * | 1994-08-24 | 1997-08-19 | Loral Corp. | Precision guidance system for aircraft launched bombs |
US5647558A (en) * | 1995-02-14 | 1997-07-15 | Bofors Ab | Method and apparatus for radial thrust trajectory correction of a ballistic projectile |
US5671138A (en) * | 1995-07-06 | 1997-09-23 | The United States Of America As Represented By The Secretary Of The Navy | Fuzzy controller for acoustic vehicle target intercept guidance |
US5671139A (en) * | 1995-07-06 | 1997-09-23 | Bessacini; Anthony F. | Hierarchical fuzzy controller for beam rider guidance |
US5671140A (en) * | 1995-07-06 | 1997-09-23 | The United States Of America As Represented By The Secretary Of The Navy | Fuzzy controller for target intercept guidance |
US5828571A (en) * | 1995-08-30 | 1998-10-27 | The United States Of America As Represented By The Secretary Of The Navy | Method and apparatus for directing a pursuing vehicle to a target with evasion capabilities |
US5691531A (en) * | 1995-11-09 | 1997-11-25 | Leigh Aerosystems Corporation | Data insertion system for modulating the carrier of a radio voice transmitter with missile control signals |
US5944762A (en) * | 1996-04-01 | 1999-08-31 | The United States Of America As Represented By The Secretary Of The Navy | Hierarchical target intercept fuzzy controller with forbidden zone |
DE19651888C1 (de) * | 1996-12-13 | 1998-08-13 | Daimler Benz Aerospace Ag | System zur Endphasenführung gelenkter autonomer Flugkörper |
US5987362A (en) * | 1997-10-06 | 1999-11-16 | The United States Of America As Represented By The Secretary Of The Navy | Final approach trajectory control with fuzzy controller |
US6161061A (en) * | 1998-06-26 | 2000-12-12 | The United States Of America As Represented By The Secretary Of The Navy | Guidance controller for a minimal discrete command set |
US6845938B2 (en) * | 2001-09-19 | 2005-01-25 | Lockheed Martin Corporation | System and method for periodically adaptive guidance and control |
GB0503212D0 (en) * | 2005-02-15 | 2005-11-23 | Ultra Electronics Ltd | Improvements relating to target direction indication and acoustic pulse analysis |
US7910867B1 (en) * | 2006-03-03 | 2011-03-22 | Lockheed Martin Corporation | Architecture for a launch controller |
US7881337B2 (en) * | 2006-08-24 | 2011-02-01 | Raytheon Company | Methods and apparatus for information management systems |
IL178840A0 (en) * | 2006-10-24 | 2007-09-20 | Rafael Advanced Defense Sys | System |
US20100217899A1 (en) * | 2007-01-31 | 2010-08-26 | Raytheon Company | Munitions control unit |
US11313650B2 (en) | 2012-03-02 | 2022-04-26 | Northrop Grumman Systems Corporation | Methods and apparatuses for aerial interception of aerial threats |
US11947349B2 (en) | 2012-03-02 | 2024-04-02 | Northrop Grumman Systems Corporation | Methods and apparatuses for engagement management of aerial threats |
US9551552B2 (en) | 2012-03-02 | 2017-01-24 | Orbital Atk, Inc. | Methods and apparatuses for aerial interception of aerial threats |
US9501055B2 (en) | 2012-03-02 | 2016-11-22 | Orbital Atk, Inc. | Methods and apparatuses for engagement management of aerial threats |
US9170070B2 (en) | 2012-03-02 | 2015-10-27 | Orbital Atk, Inc. | Methods and apparatuses for active protection from aerial threats |
US10975718B2 (en) | 2013-02-12 | 2021-04-13 | Garrett Transportation I Inc | Stainless steel alloys, turbocharger turbine housings formed from the stainless steel alloys, and methods for manufacturing the same |
KR101965580B1 (ko) * | 2017-12-21 | 2019-04-04 | 주식회사 한화 | Pils 환경 모델을 기반으로 하는 유도 무기의 오작동 제어 장치 및 그 방법 |
CN112050691B (zh) * | 2020-07-23 | 2022-10-28 | 北京临近空间飞行器系统工程研究所 | 一种小型化高可靠弹载无线发射控制器 |
CN114576042B (zh) * | 2022-03-11 | 2023-06-20 | 中国工程物理研究院总体工程研究所 | 一种适用于固体火箭发动机远程点火装置及点火方法 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3987447A (en) * | 1965-06-21 | 1976-10-19 | The United States Of America As Represented By The Secretary Of The Navy | Missile command link with pulse deletion command coding |
US4093153A (en) * | 1965-11-18 | 1978-06-06 | The United States Of America As Represented By The Secretary Of The Army | Ground-controlled guided-missile system |
US4238090A (en) * | 1978-09-22 | 1980-12-09 | The United States Of America As Represented By The Secretary Of The Army | All-weather intercept of tanks from a helicopter |
FR2459955A1 (fr) * | 1979-06-27 | 1981-01-16 | Thomson Csf | Nouveau systeme de pilotage de missile et missile pilote |
FR2597226B3 (fr) * | 1986-04-09 | 1988-05-20 | Messerschmitt Boelkow Blohm | Calculateur de guidage pour une installation de lancement |
IL78757A0 (en) * | 1986-05-12 | 1986-08-31 | Israel State | Launcher for an optically guided,wire-controlled missile with improved electronic circuitry |
DE3625649A1 (de) * | 1986-07-29 | 1988-02-18 | Messerschmitt Boelkow Blohm | Einrichtung zur winkelcodierung |
FR2603695B1 (fr) * | 1986-09-09 | 1990-10-19 | Thomson Csf | Procede et dispositif de visualisation des cibles et/ou des positions des cibles utilisant des moyens d'acquisition des donnees d'un systeme d'armes |
NL8801917A (nl) * | 1988-08-02 | 1990-03-01 | Hollandse Signaalapparaten Bv | Koerscorrectiesysteem voor in baan corrigeerbare voorwerpen. |
US5080300A (en) * | 1989-12-07 | 1992-01-14 | Hughes Aircraft Company | Launcher control system for surface launched active radar missiles |
US5042742A (en) * | 1989-12-22 | 1991-08-27 | Hughes Aircraft Company | Microcontroller for controlling an airborne vehicle |
-
1990
- 1990-08-16 US US07/568,298 patent/US5118050A/en not_active Expired - Lifetime
-
1991
- 1991-07-11 CA CA002046788A patent/CA2046788A1/en not_active Abandoned
- 1991-07-21 IL IL98906A patent/IL98906A0/xx unknown
- 1991-07-25 DE DE69127414T patent/DE69127414T2/de not_active Expired - Lifetime
- 1991-07-25 EP EP91112536A patent/EP0471225B1/de not_active Expired - Lifetime
- 1991-08-13 TR TR91/0798A patent/TR26547A/xx unknown
- 1991-08-14 JP JP3204473A patent/JP2530777B2/ja not_active Expired - Lifetime
- 1991-08-15 NO NO913195A patent/NO306313B1/no not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
TR26547A (tr) | 1995-03-15 |
IL98906A0 (en) | 1992-07-15 |
US5118050A (en) | 1992-06-02 |
NO913195D0 (no) | 1991-08-15 |
EP0471225A3 (en) | 1992-09-30 |
NO306313B1 (no) | 1999-10-18 |
JP2530777B2 (ja) | 1996-09-04 |
DE69127414T2 (de) | 1998-01-02 |
CA2046788A1 (en) | 1992-02-17 |
JPH04227493A (ja) | 1992-08-17 |
NO913195L (no) | 1992-02-17 |
EP0471225B1 (de) | 1997-08-27 |
EP0471225A2 (de) | 1992-02-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8327 | Change in the person/name/address of the patent owner |
Owner name: RAYTHEON CO. (N.D.GES.D. STAATES DELAWARE), LEXING |