JPH0519723B2 - - Google Patents

Info

Publication number
JPH0519723B2
JPH0519723B2 JP58029200A JP2920083A JPH0519723B2 JP H0519723 B2 JPH0519723 B2 JP H0519723B2 JP 58029200 A JP58029200 A JP 58029200A JP 2920083 A JP2920083 A JP 2920083A JP H0519723 B2 JPH0519723 B2 JP H0519723B2
Authority
JP
Japan
Prior art keywords
signal
washout
control
actuator
generating
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
Application number
JP58029200A
Other languages
English (en)
Japanese (ja)
Other versions
JPS58166403A (ja
Inventor
Richaado Sukuuteki Edomando
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.)
Unisys Corp
Original Assignee
Unisys 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 Unisys Corp filed Critical Unisys Corp
Publication of JPS58166403A publication Critical patent/JPS58166403A/ja
Publication of JPH0519723B2 publication Critical patent/JPH0519723B2/ja
Granted legal-status Critical Current

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
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • G05D1/0833—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability using limited authority control

Landscapes

  • Engineering & Computer Science (AREA)
  • Computer Security & Cryptography (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)
  • Feedback Control In General (AREA)
JP58029200A 1982-03-09 1983-02-23 安定増大システム用適合的ウオツシユアウト装置 Granted JPS58166403A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/356,549 US4481586A (en) 1982-03-09 1982-03-09 Adaptive washout circuit for use in a stability augmentation system
US356549 1982-03-09

Publications (2)

Publication Number Publication Date
JPS58166403A JPS58166403A (ja) 1983-10-01
JPH0519723B2 true JPH0519723B2 (cg-RX-API-DMAC7.html) 1993-03-17

Family

ID=23401912

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58029200A Granted JPS58166403A (ja) 1982-03-09 1983-02-23 安定増大システム用適合的ウオツシユアウト装置

Country Status (4)

Country Link
US (1) US4481586A (cg-RX-API-DMAC7.html)
EP (1) EP0088614B1 (cg-RX-API-DMAC7.html)
JP (1) JPS58166403A (cg-RX-API-DMAC7.html)
DE (1) DE3365062D1 (cg-RX-API-DMAC7.html)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3200839C1 (de) * 1982-01-14 1983-08-25 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Vorrichtung zum Trimmen von Flugzeugen
US4659035A (en) * 1985-01-25 1987-04-21 The United States As Represented By The Secretary Of The Navy Rate estimation by mixing two independent rate signals
US5170969A (en) * 1988-11-23 1992-12-15 The Boeing Company Aircraft rudder command system
US5593109A (en) * 1995-01-10 1997-01-14 Lucas Western, Inc. Actuator system and method
US7988089B2 (en) * 2008-03-27 2011-08-02 Sikorsky Aircraft Corporation Swashplate trajectory control
CN110471290B (zh) * 2019-09-05 2022-05-27 山东科技大学 一种具有抗饱和功能的无人机直接自适应容错控制方法

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3752420A (en) * 1971-01-04 1973-08-14 Sperry Rand Corp Augmented washout circuit for use in automatic pilots
US4012018A (en) * 1973-10-04 1977-03-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration All sky pointing attitude control system
US4129275A (en) * 1974-11-22 1978-12-12 The Boeing Company Automatic flight control apparatus for aircraft
CA1050633A (en) * 1974-12-19 1979-03-13 Ronald J. Miller Semi-automatic flight control system utilizing limited authority stabilization system
US4071211A (en) * 1976-09-23 1978-01-31 Rca Corporation Momentum biased active three-axis satellite attitude control system
US4106094A (en) * 1976-12-13 1978-08-08 Turpin Systems Company Strap-down attitude and heading reference system
US4095271A (en) * 1977-04-20 1978-06-13 Sundstrand Data Control, Inc. Aircraft pitch attitude signal generator
US4294420A (en) * 1978-01-30 1981-10-13 Matra Attitude control systems for space vehicles
US4277041A (en) * 1978-09-11 1981-07-07 Lockheed Corporation Aircraft cruise speed control system
US4382283A (en) * 1980-08-08 1983-05-03 United Technologies Corporation Helicopter attitude and airspeed acquisition and retention system
US4383299A (en) * 1981-03-30 1983-05-10 United Technologies Corporation Command-inhibited aircraft attitude reference adjustment
US4385356A (en) * 1981-03-30 1983-05-24 United Technologies Corporation Non-saturating airspeed/attitude controls

Also Published As

Publication number Publication date
US4481586A (en) 1984-11-06
DE3365062D1 (en) 1986-09-11
JPS58166403A (ja) 1983-10-01
EP0088614A1 (en) 1983-09-14
EP0088614B1 (en) 1986-08-06

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