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특허 상세정보

System and method for an integrated backup control system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-013/00    B64C-013/42   
미국특허분류(USC) 244/194; 244/221; 244/229; 244/099.4
출원번호 US-0019226 (2011-02-01)
등록번호 US-8104720 (2012-01-31)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Ingrassia Fisher & Lorenz, P.C.
인용정보 피인용 횟수 : 11  인용 특허 : 71
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

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 having at least one processor configured to generate a tactile signal for the actuated control stick;a set of primary electronics coupled to the primary sensor and located in the processing unit, the set of primary electronics being configured to receive a primary control stick signal from the primary sensor and to generate at least one primary control signal ...

이 특허에 인용된 특허 (71)

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이 특허를 인용한 특허 피인용횟수: 11

  1. Ahmed, Ghufran; Ferik, Sami El. Adaptive control method for unmanned vehicle with slung load. USP2015099146557.
  2. Richter, Martin; Lücken, Peter. Aircraft having a vertical lift system. USP2016029266605.
  3. Omar, Hanafy M.. Control optimization method for helicopters carrying suspended loads. USP2012058190307.
  4. Fervel, Marc; Lecanu, Arnaud; Maussion, Antoine; Aubert, Jean-Jacques. Distributed flight control system implemented according to an integrated modular avionics architecture. USP2015079081372.
  5. Srebranig, Steven. Fault tolerant system with equivalence processing driving fault detection and backup activation. USP2015119197934.
  6. Oltheten, Erik; McCollough, James M.; Scheidler, Peter F.; Greenwood, Jeffery S.. Fly-by-wire engine power control system. USP2015089096325.
  7. Omar, Hanafy M.. Fuzzy logic-based control method for helicopters carrying suspended loads. USP2012058185259.
  8. 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.
  9. Ahmad, Zafar S.; Roltgen, John W.; Singer, Mark C.; Bader, Douglas L.. Triplex cockpit control data acquisition electronics. USP2014048690101.
  10. Hagerott, Steven G.; Klausmeyer, Steven; Mendoza, Gonzalo E.. Yaw damping system and method for aircraft. USP2013128620492.
  11. Hagerott, Steven G.; Klausmeyer, Steven; Mendoza, Gonzalo E.. Yaw damping system and method for aircraft. USP2014108874286.