ATE287553T1 - Flugzeugsteuersystem - Google Patents

Flugzeugsteuersystem

Info

Publication number
ATE287553T1
ATE287553T1 AT01910010T AT01910010T ATE287553T1 AT E287553 T1 ATE287553 T1 AT E287553T1 AT 01910010 T AT01910010 T AT 01910010T AT 01910010 T AT01910010 T AT 01910010T AT E287553 T1 ATE287553 T1 AT E287553T1
Authority
AT
Austria
Prior art keywords
aircraft
control system
excitation
rigid body
aircraft control
Prior art date
Application number
AT01910010T
Other languages
English (en)
Inventor
Ian Thomas Darbyshire
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 ATE287553T1 publication Critical patent/ATE287553T1/de

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, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Traffic Control Systems (AREA)
  • Feedback Control In General (AREA)
  • Selective Calling Equipment (AREA)
  • Radio Relay Systems (AREA)
  • Air Conditioning Control Device (AREA)
  • Flow Control (AREA)
  • Sorption Type Refrigeration Machines (AREA)
AT01910010T 2000-03-29 2001-03-08 Flugzeugsteuersystem ATE287553T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
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 (1)

Publication Number Publication Date
ATE287553T1 true ATE287553T1 (de) 2005-02-15

Family

ID=9888667

Family Applications (1)

Application Number Title Priority Date Filing Date
AT01910010T ATE287553T1 (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 (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007001372A2 (en) 2004-09-17 2007-01-04 Aurora Flight Sciences Ducted spinner for engine cooling
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
US7506837B2 (en) 2004-09-17 2009-03-24 Aurora Flight Sciences Corporation Inbound transition control for a tail-sitting vertical take off and landing aircraft
US7364115B2 (en) 2004-09-17 2008-04-29 Aurora Flight Sciences Corporation 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
CA2906409C (en) 2013-03-15 2020-01-07 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
WO2001073516A1 (en) 2001-10-04
DE60108498T2 (de) 2005-06-30
AU2001237594A1 (en) 2001-10-08
US20030141418A1 (en) 2003-07-31
EP1290518A1 (de) 2003-03-12
EP1290518B1 (de) 2005-01-19
GB0007619D0 (en) 2000-05-17
US6986486B2 (en) 2006-01-17
DE60108498D1 (de) 2005-02-24
ES2231451T3 (es) 2005-05-16

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Legal Events

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RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties