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System and method for an integrated backup control system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-013/00   
미국특허분류(USC) 244/223; 244/0994; 244/228; 244/229; 244/236
출원번호 US-0654474 (2007-01-17)
등록번호 US7878461 (2011-01-18)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    King & Spalding LLP
인용정보 피인용 횟수 : 15  인용 특허 : 70
초록
▼

Embodiments of the invention relate to a flight control system for controlling an aircraft in flight having a backup control system integrated into an active control stick. The actuated control stick may include a processing unit that includes independent and separate hardware and/or software dedicated to the primary control system and the backup control system. For the primary control system, the processing unit may receive a sensed primary control stick signal and communicate with a primary processor, which may be configured to generate a primary contr...

대표
청구항
▼

What is claimed is: 1. A flight control system for controlling an aircraft in flight, the flight control system comprising:an actuated control stick comprising a primary sensor, a backup sensor, and a processing unit, the processing unit comprising at least one processor configured to generate a tactile signal for the actuated control stick, the processing unit being configured to adjust the feel of the actuated control stick based upon the tactile signal, the tactile signal generated from at least one of a primary control stick signal generated by the p...

이 특허에 인용된 특허 (70)

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이 특허를 인용한 특허 피인용횟수: 15

  1. Johnson, Andrew T.; Hanlon, Casey. Active user interface haptic feedback and linking control system using either force or position data. USP2011128078340.
  2. Higuchi, Yosuke; Matsuda, Takeshi. Aircraft and aircraft control method. USP2015089108722.
  3. Richter, Martin; Lücken, Peter. Aircraft having a vertical lift system. USP2016029266605.
  4. Hirvonen, Jukka Matti. Apparatus and method for backup control in a distributed flight control system. USP2012088235328.
  5. Antraygue, Cedric. Electronic operational control device for a piloting member with cross-monitoring, piloting device and aircraft. USP2014028659257.
  6. Hogenmueller, Thomas; Huck, Thorsten; Kersken, Ulrich; Ruehle, Armin; Tilsner, Heinz; Gebauer, Carsten; Baysal, Tuelin; Mueller, Bernd; Blaschke, Volker; Niem, Wolfgang. Fail-safe EE architecture for automated driving. USP2017039606537.
  7. Olsoe, Jonathan S.; McLaughlin, David; Hartin, Charles B.; Cyrot, Luc; Streeter, Bruce; Wanchu, Stephane. Flight control system with alternate control path. USP2015018935015.
  8. Shue, Shyhpyng Jack; Corrigan, John James; Bird, Eric Thomas; Wood, Tommie Lynn; Ewing, Alan Carl. Method and apparatus for aircraft sensor and actuator failure protection using reconfigurable flight control laws. USP2014078763950.
  9. Shue, Shyhpyng Jack; Corrigan, John James; Bird, Eric Thomas; Wood, Tommie Lynn; Ewing, Alan Carl. Method and apparatus for aircraft sensor and actuator failure protection using reconfigurable flight control laws. USP2017079701404.
  10. Shue, Shyhpyng Jack; Corrigan, John James; Bird, Eric Thomas; Wood, Tommie Lynn; Ewing, Alan Carl. Method and apparatus for aircraft sensor and actuator failure protection using reconfigurable flight control laws. USP20190110183743.
  11. Szulyk, Zenon P.; Jayaraman, Ganga P.; Frayman, Charles C.; Dyra, Brian P.; Stachniak, Darryl S.. Position control system for cross coupled operation of fly-by-wire control columns. USP2014088814103.
  12. Hirvonen, Jukka Matti; Palfreyman, Gary. System and method for an integrated backup control system. USP2012018104720.
  13. Ahmad, Zafar S.; Roltgen, John W.; Singer, Mark C.; Bader, Douglas L.. Triplex cockpit control data acquisition electronics. USP2014048690101.
  14. Hagerott, Steven G.; Klausmeyer, Steven; Mendoza, Gonzalo E.. Yaw damping system and method for aircraft. USP2013128620492.
  15. Hagerott, Steven G.; Klausmeyer, Steven; Mendoza, Gonzalo E.. Yaw damping system and method for aircraft. USP2014108874286.

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