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특허 상세정보

Process and system for piloting an aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) G05D-003/00   
미국특허분류(USC) 244/195; 244/076.R; 701/011
출원번호 US-0458751 (2003-06-11)
우선권정보 FR-0007197 (2002-06-12)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Stevens, Davis, Miller &
인용정보 피인용 횟수 : 4  인용 특허 : 10

The piloting system (1) for generating orders for piloting the aircraft according to at least one piloting axis, for example the pitch axis, the roll axis, the yaw axis or the engine thrust control axis, comprises at least two piloting means (2, 3), each of which is capable of calculating the derivative with respect to time of the function which represents the corresponding piloting law and which takes into account the current values of parameters of the aircraft, first means (4) for intercomparing the derivatives calculated by the piloting means (2, 3) ...


1. A process for piloting an aircraft by generating orders for piloting said aircraft on at least one piloting axis using at least two different piloting laws, which relate to said piloting axis and which each are used to determine the piloting orders as a function of parameters of the aircraft, wherein, for said piloting axis, the following operations are carried out automatically and repetitively:a) for each of said piloting laws, the derivative with respective to time of a function which corresponds to said piloting law and which takes into account th...

이 특허에 인용된 특허 (10)

  1. Najmabadi Kioumars ; Evans Monte R. ; Coleman Edward E. ; Bleeg Robert J. ; Breuhaus Richard S. ; Anderson Dorr Marshall ; Nelson Timothy A.. Aircraft pitch-axis stability and command augmentation. USP1998035722620.
  2. Najmabadi Kioumars ; Evans Monte R. ; Bleeg Robert J. ; Breuhaus Richard S.. Aircraft pitch-axis stability and command augmentation system. USP1999115979835.
  3. Morgan Charles P. (Marion IA) Lamy Jean L. (Cedar Rapids IA). Control of positioning system authority over aircraft control surfaces as a function of surface movement rate. USP1977064032094.
  4. Osder Stephen S. (Scottsdale AZ). Dynamic equalization system for dual channel automatic pilot. USP1980064209734.
  5. Vos David W. (Boston MA). Fault tolerant automatic control system utilizing analytic redundancy. USP1997035615119.
  6. Lyloc Woon (Cedar Rapids) Pattison David C. (Cedar Rapids IA). Fly by wire/fly by light control system with manual override. USP1993035197697.
  7. Hhner Herbert (Neu Anspach DEX) Kesberg Jrgen (Nidderau DEX). Method and circuit configuration for forming an evaluation signal from a plurality of redundant measurement signals. USP1993085233542.
  8. Larramendy Panxika,FRX ; Delgado Daniel,FRX. Method for protecting an aircraft against vertical gusts of wind and pitch-attitude control device employing this method. USP2000036044311.
  9. Steglich Helmar Rudolf (Marblehead MA). System for generating an angular rate signal from an angular position signal utilizing a constant amplitude-variable car. USP1977034011440.
  10. Farineau Jacques (Toulouse FRX) Larramendy Panxika (Toulouse FRX). System for integrated pitch and thrust control of an aircraft. USP1992075127608.