DE3750161D1 - Flugsteuerungssystem mit synthetischer geschwindigkeitsstabilisierung. - Google Patents

Flugsteuerungssystem mit synthetischer geschwindigkeitsstabilisierung.

Info

Publication number
DE3750161D1
DE3750161D1 DE3750161T DE3750161T DE3750161D1 DE 3750161 D1 DE3750161 D1 DE 3750161D1 DE 3750161 T DE3750161 T DE 3750161T DE 3750161 T DE3750161 T DE 3750161T DE 3750161 D1 DE3750161 D1 DE 3750161D1
Authority
DE
Germany
Prior art keywords
control system
flight control
speed stabilization
synthetic speed
synthetic
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 - Fee Related
Application number
DE3750161T
Other languages
English (en)
Other versions
DE3750161T2 (de
Inventor
Jean Boudreau
Howard Berman
Jimmie Chin
Romeo Martorella
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Grumman Corp
Original Assignee
Grumman Aerospace Corp
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 Grumman Aerospace Corp filed Critical Grumman Aerospace Corp
Publication of DE3750161D1 publication Critical patent/DE3750161D1/de
Application granted granted Critical
Publication of DE3750161T2 publication Critical patent/DE3750161T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
    • B64C13/18—Initiating means actuated automatically, e.g. responsive to gust detectors using automatic pilot
    • 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
    • G05D1/0623—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind by acting on the pitch

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE3750161T 1986-10-27 1987-10-22 Flugsteuerungssystem mit synthetischer geschwindigkeitsstabilisierung. Expired - Fee Related DE3750161T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/923,243 US4767085A (en) 1986-10-27 1986-10-27 Synthetic speed stability flight control system
PCT/US1987/002714 WO1988003112A1 (en) 1986-10-27 1987-10-22 Synthetic speed stability flight control system

Publications (2)

Publication Number Publication Date
DE3750161D1 true DE3750161D1 (de) 1994-08-04
DE3750161T2 DE3750161T2 (de) 1994-11-03

Family

ID=25448367

Family Applications (1)

Application Number Title Priority Date Filing Date
DE3750161T Expired - Fee Related DE3750161T2 (de) 1986-10-27 1987-10-22 Flugsteuerungssystem mit synthetischer geschwindigkeitsstabilisierung.

Country Status (7)

Country Link
US (1) US4767085A (de)
EP (1) EP0290532B1 (de)
JP (1) JP2656052B2 (de)
CA (1) CA1328911C (de)
DE (1) DE3750161T2 (de)
IL (1) IL84277A (de)
WO (1) WO1988003112A1 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5722620A (en) * 1995-05-15 1998-03-03 The Boeing Company Aircraft pitch-axis stability and command augmentation
US7742846B2 (en) * 2006-06-02 2010-06-22 Sikorsky Aircraft Corporation Surface contact override landing scheme for a FBW rotary-wing aircraft
US7949440B2 (en) * 2006-12-22 2011-05-24 Embraer-Empresa Brasileira De Aeronautica S.A. Aircraft cruise speed control
US7774106B2 (en) * 2006-12-22 2010-08-10 Pratt - Whitney Canada Corp. Cruise control FADEC logic
CN100541372C (zh) * 2008-03-31 2009-09-16 北京航空航天大学 一种无人机发动机意外停车下的自动归航控制方法
US9085371B2 (en) * 2008-11-20 2015-07-21 The Boeing Company Automatic throttle roll angle compensation
US9058040B2 (en) * 2009-02-27 2015-06-16 The Boeing Company Automatic pilot pitch angle compensation
US9506945B2 (en) 2014-06-10 2016-11-29 Sikorsky Aircraft Corporation Rotorcraft flight parameter estimation
US10671090B2 (en) * 2017-09-01 2020-06-02 Embraer S.A. Automatic command for lift control devices

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2766953A (en) * 1951-07-16 1956-10-16 Honeywell Regulator Co Flight scheduling apparatus
US2799461A (en) * 1954-05-28 1957-07-16 Collins Radio Co Automatic air speed control
GB1154372A (en) * 1965-06-12 1969-06-04 Elliott Brothers London Ltd Improvements relating to Aircraft Automatic Pilots
US3624364A (en) * 1970-01-28 1971-11-30 Us Army Parallel speed stabilization system
US3698669A (en) * 1970-03-16 1972-10-17 Rita Ann Miller Method and apparatus for controlling the flight path angle of aircraft
US3892374A (en) * 1973-03-19 1975-07-01 Boeing Co Turbulence compensated throttle control system
US3921941A (en) * 1973-08-23 1975-11-25 King Radio Corp Aircraft rate trim system
US3908934A (en) * 1973-12-03 1975-09-30 Sperry Rand Corp Programmed gain control for aircraft throttle control system
US4032093A (en) * 1975-06-27 1977-06-28 The Boeing Company Adaptive energy management for vertical speed control of an aircraft
US4021009A (en) * 1975-07-24 1977-05-03 Sperry Rand Corporation Vertical path control for aircraft area navigation system
GB1563501A (en) * 1976-02-11 1980-03-26 Elliott Bros Aircrft instruments
US4044975A (en) * 1976-05-17 1977-08-30 Mcdonnell Douglas Corporation Aircraft speed command system
US4189119A (en) * 1977-11-22 1980-02-19 The Boeing Company Turbulence compensated throttle control system
US4189118A (en) * 1977-11-22 1980-02-19 The Boeing Company Shear detection and compensation circuit for aircraft throttle control system
US4245805A (en) * 1977-11-25 1981-01-20 The Boeing Company Turbulence compensated throttle control system for aircraft having throttle command signal path control means responsive to engine rating control and flare initiation
US4277041A (en) * 1978-09-11 1981-07-07 Lockheed Corporation Aircraft cruise speed control system
US4261537A (en) * 1979-02-28 1981-04-14 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Velocity vector control system augmented with direct lift control
US4281811A (en) * 1979-06-15 1981-08-04 Edo-Aire Mitchell Pitch trim system for aircraft
FR2532079A1 (fr) * 1982-08-18 1984-02-24 Sfena Procede et dispositif de pilotage d'un aerodyne dans le plan vertical, permettant la capture et le maintien d'une vitesse selectee, puis la transition vers une capture d'altitude
EP0120855B1 (de) * 1982-09-30 1989-01-25 The Boeing Company Flugregelsystem auf basis totaler energie
US4646243A (en) * 1983-01-13 1987-02-24 The Boeing Company Apparatus for determining the groundspeed rate of an aircraft
US4569493A (en) * 1983-03-14 1986-02-11 Grumman Aerospace Corporation Integrated multi-role variable sweep wing aircraft
US4590475A (en) * 1983-10-24 1986-05-20 The United States Of America As Represented By The Secretary Of The Army Stall avoidance system for aircraft
US4676460A (en) * 1984-11-28 1987-06-30 The Boeing Company Longitudinal stability augmentation system and method
BR8601586A (pt) * 1985-04-09 1986-12-30 Dei Tech Inc Aviao de caca tatico super agil e processo de pilotar o mesmo

Also Published As

Publication number Publication date
IL84277A (en) 1992-09-06
EP0290532A4 (de) 1989-07-11
EP0290532A1 (de) 1988-11-17
JP2656052B2 (ja) 1997-09-24
WO1988003112A1 (en) 1988-05-05
DE3750161T2 (de) 1994-11-03
EP0290532B1 (de) 1994-06-29
JPH01501786A (ja) 1989-06-22
CA1328911C (en) 1994-04-26
US4767085A (en) 1988-08-30
IL84277A0 (en) 1988-03-31

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee