DE69804859T2 - Kompensation für die steuerung der nickachse eines drehflüglers bei sättigung - Google Patents

Kompensation für die steuerung der nickachse eines drehflüglers bei sättigung

Info

Publication number
DE69804859T2
DE69804859T2 DE69804859T DE69804859T DE69804859T2 DE 69804859 T2 DE69804859 T2 DE 69804859T2 DE 69804859 T DE69804859 T DE 69804859T DE 69804859 T DE69804859 T DE 69804859T DE 69804859 T2 DE69804859 T2 DE 69804859T2
Authority
DE
Germany
Prior art keywords
swiveler
satured
compensation
controlling
nick
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 - Fee Related
Application number
DE69804859T
Other languages
English (en)
Other versions
DE69804859D1 (de
Inventor
J Gold
T Driscoll
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.)
Sikorsky Aircraft Corp
Original Assignee
Sikorsky Aircraft Corp
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 Sikorsky Aircraft Corp filed Critical Sikorsky Aircraft Corp
Application granted granted Critical
Publication of DE69804859D1 publication Critical patent/DE69804859D1/de
Publication of DE69804859T2 publication Critical patent/DE69804859T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • 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
    • G05D1/0011—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement
    • G05D1/0033—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement by having the operator tracking the vehicle either by direct line of sight or via one or more cameras located remotely from the vehicle
    • 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
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Feedback Control In General (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE69804859T 1997-12-23 1998-12-04 Kompensation für die steuerung der nickachse eines drehflüglers bei sättigung Expired - Fee Related DE69804859T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/996,692 US5971325A (en) 1997-12-23 1997-12-23 Compensation for rotorcraft pitch axis control saturation
PCT/US1998/025869 WO1999032951A1 (en) 1997-12-23 1998-12-04 Compensation for rotorcraft pitch axis control saturation

Publications (2)

Publication Number Publication Date
DE69804859D1 DE69804859D1 (de) 2002-05-16
DE69804859T2 true DE69804859T2 (de) 2002-11-28

Family

ID=25543196

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69804859T Expired - Fee Related DE69804859T2 (de) 1997-12-23 1998-12-04 Kompensation für die steuerung der nickachse eines drehflüglers bei sättigung

Country Status (8)

Country Link
US (1) US5971325A (de)
EP (1) EP1042707B1 (de)
JP (1) JP2001526997A (de)
AU (1) AU747638B2 (de)
CA (1) CA2316244A1 (de)
DE (1) DE69804859T2 (de)
IL (1) IL136870A (de)
WO (1) WO1999032951A1 (de)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2808339B1 (fr) * 2000-04-26 2003-06-13 Valeo Electronique Vehicule, en particulier vehicule automobile, equipe d'un systeme permettant de commander un ouvrant a distance et systeme permettant la realisation d'une telle commande
EP1307797B2 (de) * 2000-05-17 2009-04-08 The Boeing Company Intuitives fahrzeug und maschinensteuerung
US6648269B2 (en) 2001-12-10 2003-11-18 Sikorsky Aircraft Corporation Trim augmentation system for a rotary wing aircraft
US6694228B2 (en) 2002-05-09 2004-02-17 Sikorsky Aircraft Corporation Control system for remotely operated vehicles for operational payload employment
US6774860B2 (en) * 2002-05-15 2004-08-10 Northrop Grumman Corporation UAV (unmanned air vehicle) servoing dipole
US7463956B2 (en) * 2003-07-03 2008-12-09 The Boeing Company Constant vertical state maintaining cueing system
FR2876468B1 (fr) * 2004-10-08 2007-08-17 Eurocopter France Systeme de pilotage automatique d'un helicoptere
US7642975B2 (en) * 2008-03-12 2010-01-05 Sikorsky Aircraft Corporation Frame assembly for electrical bond
US9317042B2 (en) * 2014-01-28 2016-04-19 Sikorsky Aircraft Corporation Pitch feedback control splitting for helicopters with redundant actuators
US10488870B2 (en) 2015-04-16 2019-11-26 Sikorsky Aircraft Corporation Gust alleviating control for a coaxial rotary wing aircraft
US10144504B1 (en) 2017-09-01 2018-12-04 Kitty Hawk Corporation Decoupled hand controls for aircraft with vertical takeoff and landing and forward flight capabilities
CN110187634B (zh) * 2018-02-23 2023-01-31 北京京东乾石科技有限公司 飞行器的控制方法、装置和计算机可读存储介质
US11092136B2 (en) * 2018-05-04 2021-08-17 Raytheon Technologies Corporation Systems and methods for optimal speed protection for power turbine governing
WO2020068666A1 (en) * 2018-09-24 2020-04-02 Dolby Laboratories Licensing Corporation Image denoising in sdr to hdr image conversion

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5515359B2 (de) * 1974-11-22 1980-04-23
US4071811A (en) * 1976-03-01 1978-01-31 Arlyle Floyd Irwin Model helicopter throttle governor/collective pitch control apparatus
US4032083A (en) * 1976-04-12 1977-06-28 United Technologies Corporation Automatic gain control for stability augmentation systems
US4420808A (en) * 1980-04-01 1983-12-13 United Technologies Corporation Multi-axis force stick, self-trimmed aircraft flight control system
US4628455A (en) * 1983-05-06 1986-12-09 Sperry Corporation Cross axis torque limiter for helicopter autopilot
US5058824A (en) * 1989-12-21 1991-10-22 United Technologies Corporation Servo control system for a co-axial rotary winged aircraft
US5152478A (en) * 1990-05-18 1992-10-06 United Technologies Corporation Unmanned flight vehicle including counter rotating rotors positioned within a toroidal shroud and operable to provide all required vehicle flight controls
DE69217229T2 (de) * 1991-08-28 1997-06-12 United Technologies Corp., Hartford, Conn. System zur vertikalen steuerung für drehflügelflugzeug
US5552983A (en) * 1994-03-02 1996-09-03 United Technologies Corporation Variable referenced control system for remotely operated vehicles
US5429089A (en) * 1994-04-12 1995-07-04 United Technologies Corporation Automatic engine speed hold control system

Also Published As

Publication number Publication date
AU1805699A (en) 1999-07-12
AU747638B2 (en) 2002-05-16
IL136870A (en) 2004-06-20
US5971325A (en) 1999-10-26
CA2316244A1 (en) 1999-07-01
IL136870A0 (en) 2001-06-14
WO1999032951A1 (en) 1999-07-01
JP2001526997A (ja) 2001-12-25
EP1042707B1 (de) 2002-04-10
EP1042707A1 (de) 2000-10-11
DE69804859D1 (de) 2002-05-16

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee