DE60108498D1 - Flugzeugsteuersystem - Google Patents

Flugzeugsteuersystem

Info

Publication number
DE60108498D1
DE60108498D1 DE60108498T DE60108498T DE60108498D1 DE 60108498 D1 DE60108498 D1 DE 60108498D1 DE 60108498 T DE60108498 T DE 60108498T DE 60108498 T DE60108498 T DE 60108498T DE 60108498 D1 DE60108498 D1 DE 60108498D1
Authority
DE
Germany
Prior art keywords
aircraft
control system
excitation
air control
rigid body
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
DE60108498T
Other languages
English (en)
Other versions
DE60108498T2 (de
Inventor
Ian Thomas Darbyshire
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BAE Systems PLC
Original Assignee
BAE Systems PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by BAE Systems PLC filed Critical BAE Systems PLC
Application granted granted Critical
Publication of DE60108498D1 publication Critical patent/DE60108498D1/de
Publication of DE60108498T2 publication Critical patent/DE60108498T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D19/00—Control of mechanical oscillations, e.g. of amplitude, of frequency, of phase
    • G05D19/02—Control of mechanical oscillations, e.g. of amplitude, of frequency, of phase characterised by the use of electric means
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/0055—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements
DE60108498T 2000-03-29 2001-03-08 Flugzeugsteuersystem Expired - Lifetime DE60108498T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB0007619 2000-03-29
GBGB0007619.0A GB0007619D0 (en) 2000-03-29 2000-03-29 Aircraft control system
PCT/GB2001/001003 WO2001073516A1 (en) 2000-03-29 2001-03-08 Aircraft control system

Publications (2)

Publication Number Publication Date
DE60108498D1 true DE60108498D1 (de) 2005-02-24
DE60108498T2 DE60108498T2 (de) 2005-06-30

Family

ID=9888667

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60108498T Expired - Lifetime DE60108498T2 (de) 2000-03-29 2001-03-08 Flugzeugsteuersystem

Country Status (8)

Country Link
US (1) US6986486B2 (de)
EP (1) EP1290518B1 (de)
AT (1) ATE287553T1 (de)
AU (1) AU2001237594A1 (de)
DE (1) DE60108498T2 (de)
ES (1) ES2231451T3 (de)
GB (1) GB0007619D0 (de)
WO (1) WO2001073516A1 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007001371A2 (en) 2004-09-17 2007-01-04 Aurora Flight Sciences Vibration isolation engine mount system and method for ducted fan aircraft
WO2006137869A2 (en) * 2004-09-17 2006-12-28 Aurora Flight Sciences System and method for controlling a roll rate of a torsionally-disconnected freewing aircraft
WO2007001369A2 (en) 2004-09-17 2007-01-04 Aurora Flight Sciences System and method for controlling engine rpm of a ducted fan aircraft
US7437225B1 (en) * 2005-07-29 2008-10-14 Rockwell Collins, Inc. Flight management system
WO2014150501A1 (en) 2013-03-15 2014-09-25 Rolls-Royce North American Technologies, Inc. Integrated health management approach to propulsion control system protection limiting
WO2015108586A2 (en) * 2013-10-21 2015-07-23 Kespry, Inc. System and methods for execution of recovery actions on an unmanned aerial vehicle
US9701418B2 (en) 2015-10-06 2017-07-11 Honeywell International Inc. Pilot fatigue detection system and method from aircraft control device movement
US10228692B2 (en) 2017-03-27 2019-03-12 Gulfstream Aerospace Corporation Aircraft flight envelope protection and recovery autopilot
CN109292101B (zh) * 2018-11-07 2021-08-27 南通理工学院 一种无人机飞行稳定控制系统及方法

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2985409A (en) * 1955-09-26 1961-05-23 North American Aviation Inc Gust alleviation system
US3074385A (en) 1958-05-15 1963-01-22 Gen Dynamics Corp Dynamic testing apparatus
US3734432A (en) * 1971-03-25 1973-05-22 G Low Suppression of flutter
EP0067548A1 (de) 1981-06-02 1982-12-22 M.L. Aviation Company Limited Schwingungsdämpfer
JPH0211496A (ja) 1988-06-28 1990-01-16 Nec Corp 無人飛行機発射装置
US4906990A (en) 1989-02-21 1990-03-06 The Boeing Company Anti-G system failure detection
AU5507790A (en) 1989-06-20 1991-01-03 Allison, Henrikh In-flight and on-ground dynamic test device for continuous monitoring of structural integrity of pressurized aircrafts
GB2234353B (en) 1989-07-28 1994-06-01 James Ormond Beaumont Incipient failure detector
FR2656585B1 (fr) * 1989-12-28 1995-01-13 Aerospatiale Systeme pour diminuer les efforts appliques a la voilure et notamment a l'emplanture des ailes d'un aeronef en vol.
US5102072A (en) * 1990-11-19 1992-04-07 General Dynamics Corporation, Convair Division Adaptive gain and phase controller for autopilot for a hypersonic vehicle
GB2267470B (en) 1992-06-03 1995-12-13 Westland Helicopters Method and apparatus for in-flight shake testing of an aircraft fuselage
US5615119A (en) * 1995-06-07 1997-03-25 Aurora Flight Sciences Corporation Fault tolerant automatic control system utilizing analytic redundancy
JP2733046B2 (ja) 1996-03-18 1998-03-30 株式会社コミュータヘリコプタ先進技術研究所 スキッド式航空機の接地検出装置
US6622972B2 (en) * 2001-10-31 2003-09-23 The Boeing Company Method and system for in-flight fault monitoring of flight control actuators

Also Published As

Publication number Publication date
ES2231451T3 (es) 2005-05-16
DE60108498T2 (de) 2005-06-30
EP1290518A1 (de) 2003-03-12
US20030141418A1 (en) 2003-07-31
EP1290518B1 (de) 2005-01-19
ATE287553T1 (de) 2005-02-15
AU2001237594A1 (en) 2001-10-08
GB0007619D0 (en) 2000-05-17
WO2001073516A1 (en) 2001-10-04
US6986486B2 (en) 2006-01-17

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition