DE69217229D1 - System zur vertikalen steuerung für drehflügelflugzeug - Google Patents

System zur vertikalen steuerung für drehflügelflugzeug

Info

Publication number
DE69217229D1
DE69217229D1 DE69217229T DE69217229T DE69217229D1 DE 69217229 D1 DE69217229 D1 DE 69217229D1 DE 69217229 T DE69217229 T DE 69217229T DE 69217229 T DE69217229 T DE 69217229T DE 69217229 D1 DE69217229 D1 DE 69217229D1
Authority
DE
Germany
Prior art keywords
control system
vertical control
turning plane
turning
plane
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
DE69217229T
Other languages
English (en)
Other versions
DE69217229T2 (de
Inventor
Phillip Gold
Lorren Stilles
Joseph Post
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies 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 United Technologies Corp filed Critical United Technologies Corp
Application granted granted Critical
Publication of DE69217229D1 publication Critical patent/DE69217229D1/de
Publication of DE69217229T2 publication Critical patent/DE69217229T2/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 or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0661—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for take-off
    • G05D1/0669—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for take-off specially adapted for vertical take-off
DE69217229T 1991-08-28 1992-07-31 System zur vertikalen steuerung für drehflügelflugzeug Expired - Fee Related DE69217229T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US75143591A 1991-08-28 1991-08-28
PCT/US1992/006406 WO1993005457A1 (en) 1991-08-28 1992-07-31 Vertical control system for rotary wing aircraft

Publications (2)

Publication Number Publication Date
DE69217229D1 true DE69217229D1 (de) 1997-03-13
DE69217229T2 DE69217229T2 (de) 1997-06-12

Family

ID=25021972

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69217229T Expired - Fee Related DE69217229T2 (de) 1991-08-28 1992-07-31 System zur vertikalen steuerung für drehflügelflugzeug

Country Status (6)

Country Link
US (1) US5428543A (de)
EP (1) EP0601000B1 (de)
CA (1) CA2114022C (de)
DE (1) DE69217229T2 (de)
ES (1) ES2099832T3 (de)
WO (1) WO1993005457A1 (de)

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US5971325A (en) * 1997-12-23 1999-10-26 Sikorsky Aircraft Corporation Compensation for rotorcraft pitch axis control saturation
JP3166703B2 (ja) * 1998-03-27 2001-05-14 双葉電子工業株式会社 遠隔制御ヘリコプタ用ジャイロ装置
US6012676A (en) * 1998-03-31 2000-01-11 Sikorsky Aircraft Corporation Integrated fire and flight control system with automatic engine torque limiting
US6145428A (en) * 1998-03-31 2000-11-14 Sikorsky Aircraft Corporation Integrated fire and flight control system for controlling the angle of attack of a rotary wing aircraft
JP3195918B2 (ja) * 1999-03-12 2001-08-06 株式会社コミュータヘリコプタ先進技術研究所 ヘリコプタ用飛行制御装置
FR2802656B1 (fr) * 1999-12-16 2002-02-15 Eurocopter France Systeme de commande de vol pour aeronef a voilure tournante, notamment pour helicoptere
FR2809372B1 (fr) * 2000-05-29 2002-09-20 Aerospatiale Matra Airbus Aeronef a commandes de vol electriques, pourvu d'un pilote automatique
US6371408B1 (en) * 2000-08-03 2002-04-16 Dennis Halwes Helicopter tail rotor authority altitude compensator
FR2830630B1 (fr) * 2001-10-05 2004-07-30 Eurocopter France Dispositif de pilotage automatique d'un helicoptere et systeme de pilotage automatique comportant un tel dispositif
US6648269B2 (en) 2001-12-10 2003-11-18 Sikorsky Aircraft Corporation Trim augmentation system for a rotary wing aircraft
US6679458B2 (en) * 2002-06-10 2004-01-20 The Boeing Company Split detent tactile cueing vehicle control system
US7463956B2 (en) * 2003-07-03 2008-12-09 The Boeing Company Constant vertical state maintaining cueing system
US9851723B2 (en) * 2004-07-29 2017-12-26 Textron Innovations Inc. Method and apparatus for flight control of tiltrotor aircraft
US20060049303A1 (en) * 2004-08-23 2006-03-09 Wilkerson Darrell W Mechanical density altitude compensation device for helicopter tail rotors
FR2876468B1 (fr) * 2004-10-08 2007-08-17 Eurocopter France Systeme de pilotage automatique d'un helicoptere
FR2883257B1 (fr) * 2005-03-18 2007-06-01 Thales Sa Dispositif de compensation de jeu mecanique de commande de vol d'helicoptere
US8223009B2 (en) * 2006-05-15 2012-07-17 TRACK America Mobile asset tracking system and method
US8725321B2 (en) * 2006-05-17 2014-05-13 Textron Innovations Inc. Flight control system
US9340278B2 (en) 2006-05-17 2016-05-17 Textron Innovations, Inc. Flight control system
US7742846B2 (en) * 2006-06-02 2010-06-22 Sikorsky Aircraft Corporation Surface contact override landing scheme for a FBW rotary-wing aircraft
US7438259B1 (en) * 2006-08-16 2008-10-21 Piasecki Aircraft Corporation Compound aircraft control system and method
US7970498B2 (en) 2007-06-01 2011-06-28 Sikorsky Aircraft Corporation Model based sensor system for loads aware control laws
US8002220B2 (en) * 2007-10-25 2011-08-23 Honeywell International Inc. Rate limited active pilot inceptor system and method
US8275500B2 (en) * 2008-03-11 2012-09-25 Honeywell International Inc. Gas turbine engine fixed collective takeoff compensation control system and method
US8271151B2 (en) 2008-03-31 2012-09-18 Sikorsky Aircraft Corporation Flight control system for rotary wing aircraft
WO2010039386A2 (en) * 2008-10-02 2010-04-08 Carrier Corporation Refrigerant system with adaptive hot gas reheat
ES2359325B1 (es) * 2008-10-17 2012-03-23 Heribert Soler Canela Sistema para controlar la operación de una aeronave convertible entre modos helicóptero, autogiro y avión.
ITTO20090079U1 (it) * 2009-06-10 2010-12-11 Agusta Spa Sistema per la gestione ed il controllo della velocita' di uno o piu' rotori di un aeromobile atto a volare a punto fisso
FR2948629B1 (fr) * 2009-07-28 2011-08-19 Eurocopter France Amortissement variable de restitution haptique pour chaine cinematique de changement d'attitude de vol d'un aeronef
FR2950170B1 (fr) * 2009-09-16 2011-10-14 Airbus Operations Sas Methode de generation de fichiers de configuration d'interface pour calculateurs d'une plateforme avionique
DE102010022200A1 (de) * 2010-05-20 2011-11-24 Liebherr-Aerospace Lindenberg Gmbh Steuerknüppelsystem
US8190307B2 (en) 2010-08-23 2012-05-29 King Fahd University Of Petroleum & Minerals Control optimization method for helicopters carrying suspended loads
CN103314336B (zh) * 2011-01-14 2016-08-10 贝尔直升机泰克斯特龙公司 用于控制竖直飞行航迹的飞行控制系统和方法
FR2981045B1 (fr) * 2011-10-10 2013-10-25 Eurocopter France Systeme de pilotage en lacet pour giravion, mettant en oeuvre un organe entraine par l'homme qui genere des commandes de vol par objectif
JP5893890B2 (ja) * 2011-10-18 2016-03-23 三菱重工業株式会社 航空機及び航空機の制御方法
US9266608B2 (en) * 2013-03-18 2016-02-23 Sikorsky Aircraft Corporation Compensating for lead-lag in rotor system
US9146557B1 (en) * 2014-04-23 2015-09-29 King Fahd University Of Petroleum And Minerals Adaptive control method for unmanned vehicle with slung load
US10676184B2 (en) 2014-08-28 2020-06-09 Sikorsky Aircraft Corporation Pitch control system for an aircraft
WO2016043943A2 (en) 2014-08-28 2016-03-24 Sikorsky Aircraft Corporation Pitch control system
US10647413B2 (en) * 2014-09-30 2020-05-12 Sikorsky Aircraft Corporation Enhanced engine load demand anticipation
PL3069990T3 (pl) * 2015-03-20 2017-06-30 Airbus Helicopters Deutschland GmbH Urządzenie generujące sztuczne odczucie siły, do systemu sterowania pojazdu, a zwłaszcza statku powietrznego
FR3065756B1 (fr) * 2017-04-28 2019-04-26 Airbus Helicopters Dispositif de regulation d'une consigne d'une vitesse de rotation d'un rotor de giravion, giravion equipe d'un tel dispositif et methode de regulation associee
US11048273B2 (en) * 2018-06-08 2021-06-29 Textron Innovations Inc. System and method for rotorcraft height control
US10967968B2 (en) 2018-11-13 2021-04-06 Textron Innovations Inc. System and method to provide descent rate limiting for an aircraft

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US4012626A (en) * 1975-04-18 1977-03-15 Sperry Rand Corporation Vertical navigation control system
US4313165A (en) * 1979-10-23 1982-01-26 United Technologies Corporation Force feel actuator with limited proportional/integral error feedback
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US4382283A (en) * 1980-08-08 1983-05-03 United Technologies Corporation Helicopter attitude and airspeed acquisition and retention system
US4645141A (en) * 1984-05-23 1987-02-24 Rockwell International Corporation Automatic flight control system
US4696445A (en) * 1986-09-18 1987-09-29 United Technologies Corporation Collective control system for a helicopter
US4924400A (en) * 1988-09-01 1990-05-08 United Technologies Corporation Arrangement for controlling the performance of bob-up/bob-down maneuvers by a helicopter
US5001646A (en) * 1988-12-19 1991-03-19 Mcdonnell Douglas Corporation Automated helicopter flight control system
US5076517A (en) * 1989-08-14 1991-12-31 United Technologies Corporation Programmable, linear collective control system for a helicopter
US5117362A (en) * 1989-12-15 1992-05-26 Honeywell Path capture forcing function generator for aircraft vertical axis control
US5156363A (en) * 1991-02-28 1992-10-20 United Technologies Corporation Helicopter collective stick of the displacement type occupying a minimum space envelope yet whose grip generates an arc of large radius
US5224664A (en) * 1991-07-22 1993-07-06 United Technologies Corporation Adaptive control system input limiting

Also Published As

Publication number Publication date
CA2114022A1 (en) 1993-03-18
CA2114022C (en) 2000-09-19
EP0601000A1 (de) 1994-06-15
DE69217229T2 (de) 1997-06-12
ES2099832T3 (es) 1997-06-01
EP0601000B1 (de) 1997-01-29
US5428543A (en) 1995-06-27
WO1993005457A1 (en) 1993-03-18

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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