DE3272040D1 - Speed command apparatus for aircraft - Google Patents
Speed command apparatus for aircraftInfo
- Publication number
- DE3272040D1 DE3272040D1 DE8282305780T DE3272040T DE3272040D1 DE 3272040 D1 DE3272040 D1 DE 3272040D1 DE 8282305780 T DE8282305780 T DE 8282305780T DE 3272040 T DE3272040 T DE 3272040T DE 3272040 D1 DE3272040 D1 DE 3272040D1
- Authority
- DE
- Germany
- Prior art keywords
- aircraft
- speed command
- command apparatus
- speed
- command
- 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
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/04—Control of altitude or depth
- G05D1/06—Rate of change of altitude or depth
- G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
- G05D1/0615—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind
- G05D1/0638—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind by combined action on the pitch and on the motors
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/04—Control of altitude or depth
- G05D1/06—Rate of change of altitude or depth
- G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
- G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Control Of Velocity Or Acceleration (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/317,823 US4488235A (en) | 1981-11-03 | 1981-11-03 | Speed control system for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3272040D1 true DE3272040D1 (en) | 1986-08-21 |
Family
ID=23235423
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8282305780T Expired DE3272040D1 (en) | 1981-11-03 | 1982-11-01 | Speed command apparatus for aircraft |
Country Status (4)
Country | Link |
---|---|
US (1) | US4488235A (de) |
EP (1) | EP0078688B1 (de) |
JP (1) | JPS5881897A (de) |
DE (1) | DE3272040D1 (de) |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5031102A (en) * | 1979-12-03 | 1991-07-09 | The Boeing Company | Method and apparatus for aircraft pitch and thrust axes control |
US4633404A (en) * | 1983-05-20 | 1986-12-30 | Sperry Corporation | Automatic deceleration of aircraft during descent |
US4672548A (en) * | 1984-09-17 | 1987-06-09 | Sperry Corporation | Speed capture in climb for aircraft |
US4750127A (en) * | 1985-10-31 | 1988-06-07 | The Boeing Company | Energy compensated target speed for aircraft descent |
US4764872A (en) * | 1986-07-16 | 1988-08-16 | Honeywell Inc. | Vertical flight path and airspeed control system for aircraft |
US5023793A (en) * | 1989-04-10 | 1991-06-11 | United Technologies Corporation | Apparatus and method for dynamic compensation of a propeller pitch speed control governor |
US5096146A (en) * | 1990-08-17 | 1992-03-17 | The Boeing Company | Apparatus and methods for controlling commanded operation of an aircraft within a predetermined flight parameter limit |
US5314147A (en) * | 1991-08-27 | 1994-05-24 | United Technologies Corporation | Helicopter engine speed enhancement during heavy rotor load and rapid descent rate maneuvering |
US5826834A (en) * | 1994-10-19 | 1998-10-27 | Honeywell Inc. | Self adaptive limiter for automatic control of approach and landing |
US6819266B2 (en) * | 2002-10-07 | 2004-11-16 | Safe Flight Instrument Corporation | System and method for reducing the speed of an aircraft |
US7451510B2 (en) * | 2003-07-25 | 2008-11-18 | Lg Electronics, Inc. | Washing machine and method of performing spinning operation |
JP2009013919A (ja) * | 2007-07-06 | 2009-01-22 | Shindengen Electric Mfg Co Ltd | 内燃機関点火装置 |
US8311687B2 (en) | 2010-07-30 | 2012-11-13 | Ge Aviation Systems Llc | Method and system for vertical navigation using time-of-arrival control |
US9676168B2 (en) | 2010-11-19 | 2017-06-13 | Lamart Corporation | Fire barrier layer and fire barrier film laminate |
CN113955129B (zh) * | 2021-09-16 | 2024-02-02 | 中国航空工业集团公司西安飞机设计研究所 | 一种自动油门马赫数控制方法 |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1161408A (en) * | 1965-11-03 | 1969-08-13 | Sperry Rand Ltd | Take-Off Director |
US3752967A (en) * | 1971-12-20 | 1973-08-14 | C Vietor | Ascent and descent slope tracker system |
US3860800A (en) * | 1972-06-19 | 1975-01-14 | Boeing Co | Automatic pitch axis control system for aircraft |
US3967799A (en) * | 1972-11-17 | 1976-07-06 | Sundstrand Data Control, Inc. | Head up display and pitch generator |
US4019702A (en) * | 1975-11-13 | 1977-04-26 | The Boeing Company | Method and apparatus for guiding a jet aircraft in a noise-abated post-takeoff climb |
GB1563501A (en) * | 1976-02-11 | 1980-03-26 | Elliott Bros | Aircrft instruments |
US4155525A (en) * | 1977-10-25 | 1979-05-22 | The Boeing Company | Maneuver detector circuit for use in autothrottle control systems having thrust and flight path control decoupling |
US4277041A (en) * | 1978-09-11 | 1981-07-07 | Lockheed Corporation | Aircraft cruise speed control system |
US4357663A (en) * | 1979-12-03 | 1982-11-02 | The Boeing Company | Method and apparatus for aircraft pitch and thrust axes control |
-
1981
- 1981-11-03 US US06/317,823 patent/US4488235A/en not_active Expired - Lifetime
-
1982
- 1982-10-22 JP JP57185925A patent/JPS5881897A/ja active Granted
- 1982-11-01 DE DE8282305780T patent/DE3272040D1/de not_active Expired
- 1982-11-01 EP EP82305780A patent/EP0078688B1/de not_active Expired
Also Published As
Publication number | Publication date |
---|---|
EP0078688A1 (de) | 1983-05-11 |
US4488235A (en) | 1984-12-11 |
JPS5881897A (ja) | 1983-05-17 |
EP0078688B1 (de) | 1986-07-16 |
JPH0567478B2 (de) | 1993-09-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8363 | Opposition against the patent | ||
8365 | Fully valid after opposition proceedings |