DK385780A - Desensibilisering af helikopter styrereaktion paa pilotens utilsigtede bevaegelse af styrepinden - Google Patents

Desensibilisering af helikopter styrereaktion paa pilotens utilsigtede bevaegelse af styrepinden

Info

Publication number
DK385780A
DK385780A DK385780A DK385780A DK385780A DK 385780 A DK385780 A DK 385780A DK 385780 A DK385780 A DK 385780A DK 385780 A DK385780 A DK 385780A DK 385780 A DK385780 A DK 385780A
Authority
DK
Denmark
Prior art keywords
pilot
stick
term
desensibilization
washed
Prior art date
Application number
DK385780A
Other languages
English (en)
Other versions
DK146588B (da
DK146588C (da
Inventor
D L Adam
R D Murphy
W C Fischer
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
Publication of DK385780A publication Critical patent/DK385780A/da
Publication of DK146588B publication Critical patent/DK146588B/da
Application granted granted Critical
Publication of DK146588C publication Critical patent/DK146588C/da

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/56—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated
    • B64C27/57—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated automatic or condition responsive, e.g. responsive to rotor speed, torque or thrust
    • 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
    • G05D1/0061—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for transition from automatic pilot to manual pilot and vice versa

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Mechanical Engineering (AREA)
  • Toys (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Catching Or Destruction (AREA)
  • Feedback Control In General (AREA)
  • Selective Calling Equipment (AREA)
  • Traffic Control Systems (AREA)
  • Mechanical Control Devices (AREA)
DK385780A 1979-01-24 1980-09-11 Styreapparat med daempning til styring af en helikopter DK146588C (da)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US06/006,314 US4279391A (en) 1979-01-24 1979-01-24 Desensitizing helicopter control response to inadvertent pilot inputs
US631479 1979-01-24
PCT/US1980/000035 WO1980001557A1 (en) 1979-01-24 1980-01-16 Desensitizing helicopter control response to in advertent pilot input
US8000035 1980-01-16

Publications (3)

Publication Number Publication Date
DK385780A true DK385780A (da) 1980-09-11
DK146588B DK146588B (da) 1983-11-14
DK146588C DK146588C (da) 1984-04-30

Family

ID=21720289

Family Applications (1)

Application Number Title Priority Date Filing Date
DK385780A DK146588C (da) 1979-01-24 1980-09-11 Styreapparat med daempning til styring af en helikopter

Country Status (11)

Country Link
US (1) US4279391A (da)
EP (1) EP0022847B1 (da)
JP (2) JPS56501445A (da)
AT (1) ATE5245T1 (da)
AU (1) AU529394B2 (da)
CA (1) CA1127133A (da)
DE (1) DE3065491D1 (da)
DK (1) DK146588C (da)
IL (1) IL59194A (da)
NO (1) NO146947C (da)
WO (1) WO1980001557A1 (da)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4417308A (en) * 1981-03-30 1983-11-22 United Technologies Corporation Dual inner loop fault inhibit of aircraft outer loop
US4387430A (en) * 1981-03-30 1983-06-07 United Technologies Corporation Pitch stick force inhibit of aircraft automatic outer loop
US4385355A (en) * 1981-03-30 1983-05-24 United Technologies Corporation Automatic outer loop centering of aircraft inner loop
US4387432A (en) * 1981-03-30 1983-06-07 United Technologies Corporation Pulsed aircraft actuator
US4387431A (en) * 1981-03-30 1983-06-07 United Technologies Corporation Roll attitude inhibit of aircraft automatic outer loop
US4741501A (en) * 1986-01-15 1988-05-03 United Technologies Corporation Preventing augmenting vertical load induced oscillations in a helicopter
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
DE102005008286A1 (de) * 2005-02-23 2006-08-24 Dürr Special Material Handling GmbH Lagervorrichtung zum Lagern von Waren
JP5594996B2 (ja) * 2009-09-14 2014-09-24 三菱重工業株式会社 航空機の操縦システム
US10843796B2 (en) 2012-02-10 2020-11-24 Merlin Technology, Inc. Rotorcraft advanced autopilot control arrangement and methods
US9150308B2 (en) 2012-02-10 2015-10-06 Merlin Technology, Inc. Rotorcraft autopilot system, components and methods

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3584814A (en) * 1967-07-18 1971-06-15 Bell Aerospace Corp Stability and control augmentation system
US3528633A (en) * 1967-11-14 1970-09-15 Siegfried Knemeyer System for controlling and stabilizing an aircraft in yaw
US3711042A (en) * 1970-07-13 1973-01-16 Na Sa Aircraft control system
US3752420A (en) * 1971-01-04 1973-08-14 Sperry Rand Corp Augmented washout circuit for use in automatic pilots
US3733039A (en) * 1971-05-20 1973-05-15 United Aircraft Corp Feel augmentation control system for helicopters
US3920966A (en) * 1974-04-29 1975-11-18 Us Air Force Blended manual-automatic control system
US4127245A (en) * 1977-04-27 1978-11-28 United Technologies Corporation Helicopter pitch rate feedback bias for pitch axis maneuvering stability and load feel

Also Published As

Publication number Publication date
EP0022847A4 (en) 1981-07-16
WO1980001557A1 (en) 1980-08-07
CA1127133A (en) 1982-07-06
NO802804L (no) 1980-09-23
JPS56501445A (da) 1981-10-08
AU5484880A (en) 1980-07-31
IL59194A (en) 1984-01-31
EP0022847A1 (en) 1981-01-28
DK146588B (da) 1983-11-14
JPH01116000U (da) 1989-08-04
NO146947C (no) 1983-01-05
NO146947B (no) 1982-09-27
DK146588C (da) 1984-04-30
DE3065491D1 (en) 1983-12-15
ATE5245T1 (de) 1983-11-15
US4279391A (en) 1981-07-21
AU529394B2 (en) 1983-06-02
EP0022847B1 (en) 1983-11-09

Similar Documents

Publication Publication Date Title
DK385780A (da) Desensibilisering af helikopter styrereaktion paa pilotens utilsigtede bevaegelse af styrepinden
BR8003067A (pt) Sistema de controle de helicoptero para posicionamento de um leme de profundidade e processo de otimizacao de voo de helicoptero por meio da atitude do estabilizador
DK272485A (da) Fremgangsmaade til eftersoegning af personer eller genstande, f.eks. paa havet, og helikopter til udoevelse af fremgangsmaaden
DE3576318D1 (de) Ultraleichtflugzeug mit freilaufendem starrfluegel.
FR2427250A1 (fr) Mecanisme de commande de systemes de stabilisation automatique d'aeronefs
IT7948484A0 (it) Perfezionamento nei servosistemi di controllo per piloti automatici di aeromobili
BR7806707A (pt) Sistema de controle de voo
BR7603176A (pt) Aparelho para controlar a trajetoria de voo vertical do aviao,em um sistema de navegacao em area
DK384284A (da) Substituerede phenylsulfonylquanidin-derivater, deres fremstilling samt anvendelse som midler til bekaempelse af ukrudt
DE3676506D1 (de) Aktives steuersystem eines flugzeuges mit biegsamem fluegel.
SE8400953D0 (sv) Manoverkraftgradientsystem
DK184579A (da) Estere af substituerede 8-hydroxy-1-phenyl-2,3,4,5-tetrahydro-1h-3-benzazepiner,fremgangsmaade til deres fremstilling samt deres anvendelse
BR8400673A (pt) Sistema para controlar a arfada de um aviao durante operacoes de decolagem e de voo em circulos
DK570183D0 (da) Benzylcarbamoylpyridinderivater med herbicid virkning,fremgangsmaade til fremstilling deraf samt anvendelse deraf til ukrudtsbekaempelse
BR7807620A (pt) Sistema de controle de transmissao
GB2136603B (en) Helicopter attitude and airspeed acquisition and retention system
Smith Input/output coupling in eigenstructure assignment
FR1269506A (fr) Système automatique de commande notamment pilote automatique d'avion
Gonzalez-Crussi ANATOMY AND OLD LACE.
HARRISON Optimal-adaptive control theory for automatic control of aircraft(Optimal adaptive control of aircraft lateral dynamics in gust presence using Pontryagin principle and cost function)
FR1141985A (fr) Dispositif améliorant la sécurité des régulateurs d'hélices d'aéronefs à commande de variation de pas hydraulique
Sensburg et al. Active flutter suppression on an F-4 F aircraft with external stores using already existing control surfaces
Klein et al. Civil tiltrotor- Flight simulation development of instrument procedures
PUCK Stressed-skin construction of glider components using glass fiber plastics
FR1148705A (fr) Dispositif de commande automatique de changement de vitesse ou de direction de mouvement, à flux magnétique similaire ou dérivé