WO1992001906A1

WO1992001906A1 - Improved head-up display systems

Info

Publication number: WO1992001906A1
Application number: PCT/GB1990/001107
Authority: WO
Inventors: John Clifford Penwill
Original assignee: The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland
Priority date: 1990-07-19
Filing date: 1990-07-19
Publication date: 1992-02-06
Also published as: JPH05509154A; DE69009500T2; GB9300547D0; EP0545919A1; EP0545919B1; ES2054363T3; US5337048A; JP3013198B2; DE69009500D1

Abstract

A head-up display system includes means generating a pitch ladder pattern having pitch bars which are straight lines with a central gap, the pitch bars representing climb angles being solid lines and the pitch bars representing dive angles being dashed lines, the pattern having a scale factor which is unity in a central region and which increases smoothly from the central region towards the extremes of the pattern, characterised in that: a) the central bar representing level flight is considerably longer than any other bar, and the lengths of the bars decrease according to a relationship with their displacement from the central bar; b) the zenith or 90° climb angle is indicated by a distinctive star symbol and the nadir or 90° dive angle is indicated by a distinctive earth symbol, and c) the pattern has two inner regions on either side of the central region, and two outer regions between the inner regions and zenith and nadir respectively, and the graduation intervals in the outer regions are considerably greater than the graduation intervals in the inner regions, so that the first graduation interval in each outer region is considerably wider than the last graduation interval in each inner region, thus providing distinctive indications of the angles at which the inner regions end and the outer regions begin.

Description

IMPROVED HEAD-UP DISPLAY SYSTEMS

This invention relates to head-up display systems for aircraft. Known head-up display systems present an aircraft symbol and a pitch ladder display. The pitch ladder is a pattern of bars, each drawn (subject to inaccuracies resulting from the sensors and instrumentation) parallel to the actual horizon and forming a scale against which the position of the aircraft symbol indicates a measure of the attitude (pitch) or climb or dive angle of the aircraft. A central bar in the pattern represents zero climb/dive angle ie level flight, and it should overlay the actual horizon as seen through the display whenever the horizon comes within the field of view of the display. It follows that the pattern must be tilted, with respect to the display centreline, by minus the bank angle of the aircraft, and the pattern centre so placed that the aircraft symbol position gives the desired climb or dive angle measurement when read against the scale formed by the pitch bars. Only a portion of the pattern will be displayed within the field of view at any instant.

In conditions of poor visibility or in aerobatic manoeuvres or high turbulence, climb-or-dive angle information is of vital importance. It is of particular importance that whenever the pilot returns his attention to the display after having any distraction or task requiring him to look elsewhere or after any violent manoeuvre, the display will give him an immediate and accurate appreciation of the bank angle and climb-or-dive angle presented so as to minimise any possibilities of misinterpretation.

The actual horizon, or the central horizon bar in the pitch ladder naturally forms a particularly useful indication by which the pilot can judge the climb-or-dive angle of his flight, but in a climb-or-dive it will soon disappear from the field of view.

When the climb-or-dive angle changes rapidly the bars in a conventional pitch ladder may appear to be written as multiple images and may all too easily be confused. To reduce these difficulties it was suggested in patent GB2179612B that the spacing of the pitch bars should be varied. The present invention is an improvement on the invention of this patent.

SUBSTITUTESHEET It is an object of the invention to provide a head-up display system to provide the pilot with very clear analogue indications of climb-dive angle which can be immediately appreciated and also to provide a particular indication of chosen climb-or-dive angles ± ₁ which will be useful as references against which climb-or-dive angles may be judged.

According to the present invention a head-up display system includes means for generating a pitch ladder pattern having pitch bars which are straight lines with a central gap, the pitch bars representing climb angles being solid lines and the pitch bars representing dive angles being dashed lines, the pattern, having a scaie factor which is unity in a central region and which increases smoothly from the central region towards the extremes of the pattern, characterised in that: a. the central bar representing level flight is considerably longer than any other bar, and the lengths of the bars decrease according to a relationship with their displacement from the central bar; b. the zenith or 0° climb angle is indicated by a distinctive star symbol and the nadir or 90° dive angle is indicated by a distinctive earth symbol, and c. the pattern has two inner regions on either side of the central region, and two outer regions between the inner regions and zenith and nadir respectively, and the graduation intervals in the outer regions are considerably greater than the graduation intervals in the inner regions, so that the first graduation interval in each outer region is considerably wider than the last graduation interval in each inner region, thus providing distinctive indications of the angles at which the inner regions end and the outer regions begin.

Preferably the zenith star symbol is shown in outline only, and the earth symbol is a circle filled by shading lines.

Preferably the central region extends to -5° and the inner regions extend to ±30°.

Preferably the graduation intervals in the outer regions are twice as large as the graduation intervals in the inner regions.

SUBSTITUTE _SHEET Preferably the scale factor varies linearly from unity at the edge of the central region to a value of about - or 5 to 1 at the zenith and nadir.

An embodiment of the invention will now be described with reference to the drawings of which

Figure 1 is a side elevation showing sight lines through the head-up display and

Figure 2 is a drawing of the preferred form of the whole pitch ladder pattern.

Figure 1 shows the pilot's eye E and his sight lines to and through the mirror M of a head-up display unit H in a condition of near-level flight. Here an increment of climb-dive angle D, is represented by a distance between bars in the central region of the pitch ladder, and the angle D subtended at the pilot's eye by this distance, is equal to the increment D^. One of the sight-lines may be the sight-line to the horizon and as shown it should overlay the pilot's view of the actual horizon, within limits due to inaccuracies of sensors and instrumentation. Outside the central region the angle D_p would be smaller than D, according to the scale factor. Near zenith or nadir D would be approximately one quarter of V

Figure 2 shows the preferred form for the whole pattern. It should be noted that only a part of this pattern will be shown in the field of view of the display at any instant, and it will be displayed on a much larger scale than it is shown in Figure 2. The short bars just below the horizon bar are advisory descent angle markers at φ - -_ " . The other pitch bars have horizon pointing legs on their outer ends, and are labelled on the lefthand end only with the climb-or-dive angles which they indicate. The pitch ladder pattern is generated by suitable graphics generation software in a suitable computer and is positioned on the head-up display so that it forms a scale of climb-dive angle against which an aircraft symbol indicates the climb-dive angle in steady flight. Preferably the positioning of the pitch ladder display is controlled as specified in a copending application to be filed on the same day as this application.

SUBSTITUTE SHEET In the inner regions of the pitch ladder pattern from ±5° to ±30° pitch bars are provided at every 5°. In the outer regions beyond ±30° there are bars at every 10°. In consequence there is a distinctively large spacing between the 30° and 40° bars, and this will be even more apparent in an actual display than it is in Figure 2. It might be thought that this could lead to confusion, because this will be similar to the spacing between the 5° and 10° bars, but.in practice there is no possibility of confusion because the pilot has other cues. In particular he will feel the forces of gravity and acceleration, which at climb-or-dive angles of ±30° will be so different from the effects or feel of near-level flight that there will be no chance of confusion. The distinctive gaps created by the large change in graduation interval therefore have no adverse effects and have a non-obvious advantage in that they provide an extra guideline which can be used like a secondary artificial "horizon" to judge climb-or-dive angles when the actual horizon and the horizon bar are outside the field of view.

The gradual increase of scale factor causes the displacement of pitch bars from the horizon bar to follow the relationship:

Pitch bar displacement = f {φ) (measured in terms of the angle subtended at the pilot's eye position) f(φ) = φ for -5 < Φ < +5°

= 5 + 25 log_e (0*8 + 0 -0 φ) for φ > 5° = -525 log_e (0*8 - 0 -O φ) for φ < -5°

SUBSTITUTE SHEET

Claims

1. A head-up display system including means for generating a pitch ladder pattern having pitch bars which are straight lines with a central gap, the pitch bars representing climb angles being solid lines and the pitch bars representing dive angles being dashed lines, the pattern having a scale factor which is unity in a central region and which increases smoothly from the central region towards the extremes of the pattern, characterised in that: a. the central bar representing level flight is considerably longer than any other bar, and the lengths of the bars decrease according to a relationship with their displacement from the central bar; b. the zenith or 90" climb angle is indicated by a distinctive star symbol and the nadir or 90° dive angle is indicated by a distinctive earth symbol, and c. the pattern has two inner regions on either side of the central region, and two outer regions between the inner regions and zenith and nadir respectively, and the graduation intervals in the outer regions are considerably greater than the graduation intervals in the inner regions, so that the first graduation interval in each outer region is considerably wider than the last graduation interval in each inner ^' region, thus providing distinctive indications of the angles at which the inner regions end and the outer regions begin.

2. A head-up display system as claimed in claim 1 and wherein the zenith star symbol is shown in outline only, and the earth symbol is a circle filled by shading lines.

3. A head-up display system as claimed in claim 1 and wherein the central region extends to ±5" and the inner regions extend to ±30".

4. A head-up display system as claimed in claim 1 and wherein the graduation intervals in the outer regions are twice as large as the graduation intervals in the inner regions.

5. A head-up display system as claimed in claim 1 and wherein the scale factor varies linearly from unity at the edge of the central region to a value of about 4*4 or to 1 at the zenith and nadir.

SUBSTITUTESHEET

6. A head-up display system as claimed in claim 1 and wherein the lengths of the pitch bars decrease according to a linear relationship with the modulus of the climb or dive angle which they represent.

7_' A head-up display system as claimed in claim 6 and wherein the ±80^β bars are about onequarter of the length of the ±5° bars.

S_UB_STITUTESHEET