GB1347030A - Steering command indicators for vehicles - Google Patents
Steering command indicators for vehiclesInfo
- Publication number
- GB1347030A GB1347030A GB1426571*[A GB1426571A GB1347030A GB 1347030 A GB1347030 A GB 1347030A GB 1426571 A GB1426571 A GB 1426571A GB 1347030 A GB1347030 A GB 1347030A
- Authority
- GB
- United Kingdom
- Prior art keywords
- symbol
- display
- altitude
- steering command
- heading
- 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
Links
- 238000006073 displacement reaction Methods 0.000 abstract 2
- 230000003247 decreasing effect Effects 0.000 abstract 1
- 230000007935 neutral effect Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/66—Arrangements or adaptations of apparatus or instruments, not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Traffic Control Systems (AREA)
- Devices For Indicating Variable Information By Combining Individual Elements (AREA)
- Navigation (AREA)
- Instrument Panels (AREA)
Abstract
1347030 Steering command indicator SAABSCANTA AB 11 May 1971 [11 May 1970] 14265/71 Heading B7W An indicator for a vehicle to display steering commands for two manoeuvre directions comprises means for displaying a trifurcate symbol whose shape, Figs. 3a-3e, 4a-4e (not shown), is indicative of the commands, the symbol comprising three straight line branches rotatable about the same centre or adjacent centres and control means responsive to a first signal for controlling equal and opposite angular displacement of first and second branches, and responsive to a second signal for controlling angular displacement of the third branch. Thus pointers 14, Fig. 9, indicate by their inclination the magnitude of climb or dive required for an aircraft to attain a given altitude, and rotation of pointer 15 indicates the angle of turn required. Roll and pitch are indicated by the inclination and vertical position of pointer 22, and altitude by markers 26. Alternatively, Fig. 7, the steering command symbol can be generated on a CRT 29a and presented in head-up display. The dashes 33 constituting the symbol may be made to move along the rows towards or away from the centre to command increased or decreased velocity respectively. In one mode of operation, Fig. 10 (not shown), the neutral axes of the display symbol are fixed with respect to the aircraft, and heading and altitude indicated on scales (38), (39) fixed with respect to the horizon. In a further mode, Fig. 11 (not shown), the horizontal axis of the symbol is maintained parallel to a generated horizon line (41).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE06389/70A SE335248B (en) | 1970-05-11 | 1970-05-11 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1347030A true GB1347030A (en) | 1974-02-13 |
Family
ID=20268551
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1426571*[A Expired GB1347030A (en) | 1970-05-11 | 1971-05-11 | Steering command indicators for vehicles |
Country Status (8)
Country | Link |
---|---|
US (1) | US3691520A (en) |
AT (1) | AT319056B (en) |
BE (1) | BE766877A (en) |
CH (1) | CH522206A (en) |
DE (1) | DE2122830C3 (en) |
FR (1) | FR2097776A5 (en) |
GB (1) | GB1347030A (en) |
SE (1) | SE335248B (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1526396A (en) * | 1974-10-03 | 1978-09-27 | Smiths Industries Ltd | Display systems |
US4158885A (en) * | 1977-11-09 | 1979-06-19 | The Boeing Company | Guidance-light display apparatus and method for in-flight link-up of two aircraft |
US4368517A (en) * | 1978-03-16 | 1983-01-11 | Bunker Ramo Corporation | Aircraft landing display system |
US4484191A (en) * | 1982-06-14 | 1984-11-20 | Vavra George S | Tactile signaling systems for aircraft |
US4825194A (en) * | 1987-05-27 | 1989-04-25 | Honeywell Inc. | Single cue flight director indicator |
DE4109016C2 (en) * | 1991-03-20 | 1994-10-06 | Dornier Luftfahrt | Display instrument for aircraft to display the flight position, in particular the roll and pitch position or the flight path angle |
US5382954A (en) * | 1993-05-27 | 1995-01-17 | Honeywell Inc. | Resolution advisory display instrument for TCAS guidance |
GB9508659D0 (en) * | 1995-04-28 | 1995-06-14 | Smiths Industries Plc | Aircraft instruments |
US6405975B1 (en) * | 1995-12-19 | 2002-06-18 | The Boeing Company | Airplane ground maneuvering camera system |
DE29721708U1 (en) * | 1997-12-09 | 1998-01-29 | Handeck, Claus G., 40721 Hilden | Driver's cab for land, air, water or space vehicles |
GB0006032D0 (en) * | 2000-03-13 | 2000-05-03 | Ncr Int Inc | Access to information networks by mobile |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2613350A (en) * | 1948-03-16 | 1952-10-07 | Sperry Corp | Flight indicating system for dirigible craft |
-
1970
- 1970-05-11 SE SE06389/70A patent/SE335248B/xx unknown
-
1971
- 1971-05-05 US US140340A patent/US3691520A/en not_active Expired - Lifetime
- 1971-05-07 BE BE766877A patent/BE766877A/en unknown
- 1971-05-07 AT AT397471A patent/AT319056B/en not_active IP Right Cessation
- 1971-05-08 DE DE2122830A patent/DE2122830C3/en not_active Expired
- 1971-05-10 CH CH682571A patent/CH522206A/en not_active IP Right Cessation
- 1971-05-10 FR FR7116833A patent/FR2097776A5/fr not_active Expired
- 1971-05-11 GB GB1426571*[A patent/GB1347030A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE2122830B2 (en) | 1973-07-05 |
BE766877A (en) | 1971-10-01 |
SE335248B (en) | 1971-05-17 |
FR2097776A5 (en) | 1972-03-03 |
DE2122830A1 (en) | 1971-11-25 |
DE2122830C3 (en) | 1974-02-07 |
AT319056B (en) | 1974-12-10 |
US3691520A (en) | 1972-09-12 |
CH522206A (en) | 1972-06-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PCNP | Patent ceased through non-payment of renewal fee |