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System for the yaw control of an aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) G05D-001/10   
미국특허분류(USC) 244/177
출원번호 US-0497397 (2000-02-03)
우선권정보 FR-0001300 (1999-02-04)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Stevens, Davis, Miller & Mosher, LLP
인용정보 피인용 횟수 : 9  인용 특허 : 11
초록
▼

The present invention relates to a system for the yaw control of an aircraft fitted with a plurality of engines, the system (SC) comprising in particular a computation unit (16) formulating a command dr for yaw control, dr=Ka..PHI.c+Kb.p+Kc..PHI.+Kd.r+Ke..beta., on the basis of the controlled roll attitude .PHI.c, of the roll rate p, of the effective roll attitude .PHI., of the yaw rate r, of the sideslip .beta. and of gains Ka, Kb, Kc, Kd and Ke which are fixed by a device (28). According to the invention, the system (SC) comprises a a device (30) for d...

대표
청구항
▼

1. A system for yaw control of an aircraft fitted with a plurality of engines, said system comprising:at least one control facility, for the yaw control, capable of being actuated by a pilot of the aircraft; first means delivering electrical signals representative respectively of the controlled roll attitude .PHI.c, of the roll rate p, of the effective roll attitude .PHI., of the yaw rate and r and of the sideslip .beta. of said aircraft; a computation unit formulating an electrical command dr for yaw control, on the basis of the relation: dr=Ka..PHI.c+K...

이 특허에 인용된 특허 (11)

  1. Wendt Hans J. (Buxtehude DEX). Control signal transmitting apparatus, particularly for aircraft. USP1983124422180.
  2. Carl Udo (Bremen DEX). Drive control for a vertical rudder of an aircraft. USP1988074759515.
  3. McCuen Michael S. (Kirkland WA). Full authority engine-out control augmentation subsystem. USP1990064935682.
  4. Chenoweth Charles C. (Bellevue WA) Shen Jan-son (Bellevue WA). Method and apparatus for cooling and replenishing aircraft hydraulic actuators. USP1992055109672.
  5. Aldrich Allyn M. (Rockford IL). Multi-motor actuation system for a power drive unit. USP1985084533097.
  6. Frerk Karl (Delmenhorst DEX). Operating the control surfaces in aircraft. USP1988124793576.
  7. Gautier Jean-Pierre,FRX ; Ortega Jean-Marc,FRX. Process and device for the control of the rudder of an aircraft. USP1998085791596.
  8. Gautier Jean-Pierre,FRX ; Ortega Jean-Marc,FRX. Process and device for the control of the rudder of an aircraft. USP2001036206329.
  9. Kennedy ; Jr. ; Thomas W.. Side slip angle command SCAS for aircraft. USP1978064094479.
  10. Kissel Gerhard K. (Ottobrunn DEX). Steering mechanism with an active force feedback, especially for aircraft. USP1980124236685.
  11. Farineau Jacques (Toulouse FRX). System for controlling roll and yaw of an aircraft. USP1990104964599.

이 특허를 인용한 특허 피인용횟수: 9

  1. Clark, Walter Dennis. Aircraft with forward opening inlay spoilers for yaw control. USP2005056892982.
  2. Ferro, Daniel. Device and method for assisting in the management of an engine failure on an aircraft. USP2012048155803.
  3. Delannoy, Stéphane; Bertin, Thierry. Method and device for piloting an aircraft about a piloting axis. USP2012038141824.
  4. Thomas,Steven H.. Methods and system for determining angles of attack and sideslip using flow sensors. USP2008057377159.
  5. Cronin, Dennis J.; Amerson, Thomas D.. Sideslip correction for a multi-function three probe air data system. USP2003086609421.
  6. Hervieux, Arnauld R. E.; Meignat, Gregory Y.. Stability and control augmentation system. USP20180710037040.
  7. Yogev, Itzhak; Shepshelovich, Michael; Abramov, Danny. System and method for an air vehicle. USP2017029561844.
  8. Hagerott, Steven G.; Klausmeyer, Steven; Mendoza, Gonzalo E.. Yaw damping system and method for aircraft. USP2013128620492.
  9. Hagerott, Steven G.; Klausmeyer, Steven; Mendoza, Gonzalo E.. Yaw damping system and method for aircraft. USP2014108874286.

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