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특허 상세정보

Apparatus and methods for maintaining aircraft track angle during an asymmetric flight condition

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-013/04    G05D-001/12   
미국특허분류(USC) 244/183 ; 244/184 ; 364/428
출원번호 US-0346436 (1989-05-01)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 27  인용 특허 : 0
초록

When an aircraft is operating in an asymmetrical flight condition, such as during a landing decrab maneuver or during inflight engine out, the pilot is normally required to make precise compensatory roll control inputs to keep the aircraft moving along its original track angle. The pilot is relieved of this compensatory roll control task by providing a control system which automatically banks the aircraft to maintain the flight of the aircraft along the selected track angle while in the asymmetrical flight condition. Further adjustments in the bank angle...

대표
청구항

An aircraft track angle hold control system comprising: a. roll control surfaces capable of generating a rolling moment on the aircraft in flight; b. yaw control means for permitting a pilot to command the aircraft to assume a nonzero sideslip condition through a rudder pedal input wherein the yaw control means includes a maneuver command control system which interprets the rudder pedal input as a sideslip angle command and which uses feedback control means to position a yaw control surface of the aircraft in such manner as to cause an actual sideslip an...

이 특허를 인용한 특허 피인용횟수: 27

  1. Wyrembek,Susanne; May,Peter; Muthreich,Klaus. Aerodynamic component for controlling a landing guide path of an aircraft. USP2006077070148.
  2. Harrigan,Jeffery S.; Beaufrere,Henry L.. Aerospace vehicle yaw generating systems and associated methods. USP2007037185859.
  3. Harrigan,Jeffery S.; Beaufrere,Henry L.. Aerospace vehicle yaw generating systems and associated methods. USP2008057367530.
  4. Greene Leonard M. (Scarsdale NY). Aircraft control system. USP1997015590853.
  5. Tran Chuong B. ; White Stephen. Aircraft frequency adaptive modal suppression system. USP1999015860625.
  6. Giazotto,Alessandro Riccardo Britannico. Aircraft mode suppression. USP2008047357357.
  7. Knoop, Sven; Galinski, Mike. Apparatus and method for testing an aircraft pedal system. USP2013078485051.
  8. Burken John J. ; Burcham ; Jr. Frank W. ; Bull John. Emergency multiengine aircraft system for lateral control using differential thrust control of wing engines. USP2000086102330.
  9. Christensen, Kevin Thomas; Shue, Shyhpyng Jack; Caudill, Troy Sheldon. Flight control laws for vertical flight path. USP2016049304516.
  10. Shultz, Peter M.; Fenny, Carlos A.; Walker, Todd; Arjunan, Sam. Mechanical flight control auxiliary power assist system. USP2010027668627.
  11. Shultz, Peter M.; Fenny, Carlos A.; Walker, Todd; Arjunan, Sam. Mechanical flight control auxiliary power assist system. USP2011027890222.
  12. 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.
  13. Colomer, Alexandre; Dal Santo, Xavier. Method and device for attenuating on an aircraft the effects of a vertical turbulence. USP2013018359130.
  14. Wyrembek,Susanne; May,Peter; Muthreich,Klaus. Method and device for steepening a landing approach of an aircraft. USP2008017316371.
  15. He, Gang; Wyatt, Ivan Sandy. Method and system displaying crosswind correction for approach to a runway. USP2013038392039.
  16. Brown Todd Allen ; Tseng Hongtei Eric. Method for detecting a bank angle experienced by a moving vehicle. USP2000066073065.
  17. Nolte Edward P. ; Myers Michael J. ; Coombs David C. ; Griffin ; III John C.. Method of automated thrust-based roll guidance limiting. USP2001086282466.
  18. Schmidt, Philip A.. Multi-engine aircraft thrust balancing. USP2018029889944.
  19. Lohmiller, Winfried. Path controller for vehicles whose path is influenced by cross currents and a path control system and associated methods. USP2003066574532.
  20. Capell ; Sr. William Jack (Westwood MA). Signal processing system and technique for calculating roll bias data. USP1997065640369.
  21. Courter, Brandon M.; Ngo, Nam V.; Farner, Scott C; Dray, Joseph M.. System and method for optical time-domain reflectometry and design data wire testing. USP20190310230459.
  22. Greene,Leonard M.. System for measuring an airflow angle at the wingtip of an aircraft. USP2008077395705.
  23. Zweifel, Terry L.. Systems and methods for aircraft windshear detection. USP2013088508387.
  24. Wittmer, Kenneth S.; Kubik, Stephen. Vehicle heading error compensation. USP20180910073455.
  25. Wittmer, Kenneth S.; Kubik, Stephen. Vehicle heading error compensation. USP2016069360869.
  26. Hagerott, Steven G.; Klausmeyer, Steven; Mendoza, Gonzalo E.. Yaw damping system and method for aircraft. USP2013128620492.
  27. Hagerott, Steven G.; Klausmeyer, Steven; Mendoza, Gonzalo E.. Yaw damping system and method for aircraft. USP2014108874286.