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특허 상세정보

Apparatus and methods for automatically maintaining aircraft track angle

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B60C-013/18   
미국특허분류(USC) 364/434 ; 364/435 ; 244/178 ; 244/181
출원번호 US-0346432 (1989-05-01)
발명자 / 주소
인용정보 피인용 횟수 : 22  인용 특허 : 10

There is provided a controller for aiding a pilot to control an airplane\s track over the ground. While the airplane is in the air, a lateral control subsystem is provided for automatically holding the aircraft aligned with a desired track angle. Control is initiated when the pilot places the airplane in a wings level condition and centers his roll axis controller (e.g., wheel or stick). An in-air track rate control subsystem is also provided. While the airplane is on the ground, a directional control subsystem is provided which enables the pilot to comm...


A control system for an aircraft, the control system comprising: a. roll input means, (i) which are movable by a pilot of the aircraft, for generating a first command signal which is a function of an input made by the pilot to the roll input means so as to control a roll angle of the aircraft and (ii) which are movable in a manner that when the roll input means are in a neutral position there is no rolling moment applied to the aircraft in response to the first command signal; b. means for generating a second command signal, as a function of a selected n...

이 특허를 인용한 특허 피인용횟수: 22

  1. Tran Chuong B. ; White Stephen. Aircraft frequency adaptive modal suppression system. USP1999015860625.
  2. Cherepinsky, Igor. Automatic trim system for fly-by-wire aircraft with unique trim controllers. USP2012078231085.
  3. Sankrithi, Mithra M. K. V.. Autotiller control system for aircraft. USP2005086928363.
  4. Morokhovskyi, Victor. Control device and method of operating the control device having controller chips and change-over unit. USP2009087573315.
  5. Huynh,Neal V.. Control surface controller force measurement system. USP2006016981409.
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  7. Hara, Akihiro. Drive system for ground spoiler, and aircraft. USP2017049630705.
  8. Gold Phillip J. (Shelton CT) Fogler ; Jr. Donald L. (Milford CT) Dryfoos James B. (Wallingford PA). Inertial velocity command system. USP1996095553812.
  9. Strickling, James Eugene. Method and apparatus for conversion of GPS heading data for use by electronic flight director. USP2015038989925.
  10. Jones, Richard D.; Speer, Thomas E.. Method and computer program product for estimating at least one state of a dynamic system. USP2004036711476.
  11. Louise, Pascale; Dupre, Alain; Atencia, Anthony; Cortet, Emmanuel; Dal Santo, Xavier. Method and device for aiding the control of guiding modes transitions of an aircraft. USP2014058731744.
  12. Scacchi, Pierre. Method and device for automatically guiding an aircraft taxiing on the ground. USP2016089429942.
  13. Villaume,Fabrice; Duprez,Jean. Method and device for piloting an aircraft. USP2007127305285.
  14. Nolte Edward P. ; Myers Michael J. ; Coombs David C. ; Griffin ; III John C.. Method of automated thrust-based roll guidance limiting. USP2001086282466.
  15. Tada, Kazunari; Furuichi, Kazushi; Minami, Yutaro. Method of controlling steering control equipment for aircraft, and steering control equipment for aircraft and aircraft provided therewith. USP2014018630750.
  16. Schmidt, Philip A.. Multi-engine aircraft thrust balancing. USP2018029889944.
  17. Kaloust Joseph H.. Stall and recovery control system. USP2001056236914.
  18. Hagerott, Steven G.; Eddy, Stephen M.; Masud, Utbah. Systems and methods for aircraft control surface hardover and disconnect protection. USP2016109463868.
  19. Dwyer, David; Gilliland, Jr., William Ray. Systems and methods for displaying heading-based leg symbology. USP2016029250098.
  20. Paielli, Russell A.. Trajectory specification for high capacity air traffic control. USP2010017650232.
  21. Hagerott, Steven G.; Klausmeyer, Steven; Mendoza, Gonzalo E.. Yaw damping system and method for aircraft. USP2013128620492.
  22. Hagerott, Steven G.; Klausmeyer, Steven; Mendoza, Gonzalo E.. Yaw damping system and method for aircraft. USP2014108874286.