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특허 상세정보

MyON담기
내보내기 페이스북 공유 카카오톡 공유

Ground state-fly state transition control for unique-trim aircraft flight control system

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-009/00    B60V-003/08   
미국특허분류(USC) 364/434 ; 364/42406 ; 364/427 ; 364/428
출원번호 US-0243796 (1994-05-17)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 39  인용 특허 : 0
초록
▼

An aircraft control system for an unique-trim, model-following system includes a feedforward shaping function that provides quickening of pilot input, and an automatic trim function that accommodates return of the cockpit controller to an unique, centered position during trimmed flight. The basic control law is reconfigured in response to the changing state of landing gear contact to support transitions between ground state and fly state conditions. The state of the landing gear is monitored continually to recognize the occurrence of initial ground conta...

대표
청구항
▼

A system for controlling an aircraft, having landing gear and defining a pitch axis, a roll axis, a yaw axis and a lift axis, during a transition between a fly state, when no landing gear contact ground, and a ground state, when landing gear contact ground, comprising: controller means for producing a control input representing a desired value of an aircraft variable, wherein said aircraft variable comprises at least one of attitude with respect to the pitch axis, attitude with respect to the roll axis, heading with respect to the yaw axis, and altitude ...

이 특허를 인용한 특허 피인용횟수: 39

  1. Cherepinsky, Igor. Automatic trim system for fly-by-wire aircraft with unique trim controllers. USP2012078231085.
  2. Eriksen, Harald; Spivak, Alexander; Sanden, Christopher. Capacitive sensors for monitoring load bearing on pins. USP2014028659307.
  3. Eriksen, Odd Harald Steen; Sanden, Christopher. Capacitive sensors for monitoring loads. USP2015018933713.
  4. Sahasrabudhe, Vineet; Greenfield, Aaron L.; Geiger, Derek; Rigsby, James. Control system for reconfigurable rotary wing aircraft. USP20180710025320.
  5. Boyksen, Guenther; Bredemeier, Kai; Frerichs, Torsten; Eckhard, Kasch; Kasdorf, Sven; Kehlenbeck, Ult; Knijnenburg, Thorsten; Neumeyer, Max; Ottilige, Kai; Steins, Frank. Device and method for providing a flight status signal. USP2012048155804.
  6. Trotter, Steven J; Sundquist, Beth L; Arslan, Fredrick R. Electrically activated aircraft landing gear control system and method. USP2012058175762.
  7. Kaloust Joseph H.. Enhanced stall and recovery control system. USP2001066246929.
  8. Mezan, Serge. Flight control device for an aircraft, in particular for a helicopter. USP2003096622065.
  9. Sahasrabudhe, Vineet; Gold, Philip J.. Fly-by-wire flight control system with electronic lead/lag damper algorithm. USP2013108548648.
  10. Nield Brian N. ; Landes Ross A. ; Evans Monte R.. Landing attitude modifier for airplane. USP1998105823479.
  11. Fogler ; Jr. Donald L. (Milford CT) Keller James F. (Media PA). Maintaining attitude error constant in Euler singularity protection. USP1997045617316.
  12. Margolin Jed. Method and apparatus for remotely piloting an aircraft. USP1999055904724.
  13. Villaume,Fabrice; Duprez,Jean. Method and device for piloting an aircraft. USP2007127305285.
  14. Khial, Karim; Howlett, James J.; Sahasrabudhe, Vineet; Yakzan, Naji S.. Method and system for detecting forces on aircraft. USP2016059327842.
  15. Khial, Karim; Howlett, James J.; Sahasrabudhe, Vineet; Yakzan, Naji S.. Method and system for detecting forces on aircraft. USP2015059026377.
  16. Khial, Karim; Howlett, James J.; Wright, Stuart C.. Method and system for detecting forces on aircraft. USP2014108862377.
  17. Schmidt, R. Kyle; Gedeon, Steven A.. Method and system for health monitoring of aircraft landing gear. USP2012098262019.
  18. Minot, Frédéric. Method for generating interface configuration files for computers of an avionic platform. USP2013028386660.
  19. Vos, David W.. Method, apparatus and design procedure for controlling multi-input, multi-output (MIMO) parameter dependent systems using feedback LTI'zation. USP2005026859689.
  20. Vos, David W.. Method, apparatus and design procedure for controlling multi-input, multi-output (MIMO) parameter dependent systems using feedback LTI'zation. USP2003036539290.
  21. Venios, Anthony; Mongereau, Stephan; Sharma, Sanjiv; Verzichelli, Gianluca; Hebborn, Andrew; Guery, Xavier. Method, apparatus or software for controlling the heading of an aircraft on the ground. USP2013068463466.
  22. Zakrzewski, Radoslaw R.; Lynch, Michael A.; Fusare, Scott T.; Hicks, Brandon; Baird, Bradley W.. Monitoring systems and methods for aircraft landing gear. USP2014088818739.
  23. Buchholz, Robert E.; Evans, Monte R.; Lee, Jonathan P.; Overton, Timothy G.; Thoreen, Adam M.. Quiet landing attitude modifier for airplane. USP2014078781653.
  24. Gonzalez Cuadrado, Miguel. Real-time simulation procedure for a helicopter rotor. USP2013118589131.
  25. Ellis, Kristopher; Gubbels, Arthur W.. Response mode for control system of piloted craft. USP2014048688295.
  26. Vallart, Jean-Baptiste; Byzery, Romeo. Rotorcraft control system, associated rotorcraft, and corresponding control method. USP2018039915954.
  27. Eriksen, Odd Harald Steen. Sensor for measuring large mechanical strains in shear or lateral translation. USP2013128607640.
  28. Eriksen, Odd Harald Steen; Stang, Lawrence Joseph; Guo, Shuwen. Sensor for measuring large mechanical strains with fine adjustment device. USP2014018627727.
  29. Kaloust Joseph H.. Stall and recovery control system. USP2001056236914.
  30. Caldeira, Fabricio Reis; Gangsaas, Dagfinn; Polati de Souza, Alvaro Vito; Martins, Eduardo da Saiva; Vita, Marco Tulio Sguerra; Filho, Jose Marcio Vieira Dias; Campos, Marcos Vinicius; Freitas, Emerson. Stall, buffeting, low speed and high attitude protection system. USP2012048165733.
  31. Caldeira, Fabricio Reis; Gangsaas, Dagfinn; Polati de Souza, Alvaro Vito; Martins, Eduardo da Silva; Vita, Marco Tulio Sguerra; Filho, Jose Marcio Vieira Dias; Campos, Marcos Vinicius; Freitas, Emerson. Stall, buffeting, low speed and high attitude protection system. USP2012078214089.
  32. Wittmer, Kenneth S.. Swashplate trajectory control. USP2011087988089.
  33. Horsager, Thomas; Haukom, Michael; Baumgarten, William; Hansen, Matthew; Freeman, Kenneth. System and method for real-time aircraft performance monitoring. USP2017029567097.
  34. Baird, Bradley W.. Systems and methods for detecting landing gear ground loads. USP20181110131419.
  35. Eriksen, Odd Harald Steen; Guo, Shuwen; Abraha, Yosief. Systems and methods for measuring angular motion. USP2012108286508.
  36. Eriksen, Odd Harald Steen; Guo, Shuwen; Lin, Chuang-Chia; Stang, Lawrence Joseph. Systems and methods for mounting landing gear strain sensors. USP2013018359932.
  37. Shue, Shyhpyng Jack. Takeoff/landing touchdown protection management system. USP2016059354635.
  38. Schulz Gerhard,DEX ; Meyer Thomas,DEX. Trimming process for adapting a simulation system to an automatically controlled reference system. USP2001096292720.
  39. Yamane,Akihiro. Unmanned helicopter, takeoff method of unmanned helicopter, and landing method of unmanned helicopter. USP2007037195200.

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