DE3065491D1 - Desensitizing helicopter control response to inadvertent pilot input - Google Patents

Desensitizing helicopter control response to inadvertent pilot input

Info

Publication number
DE3065491D1
DE3065491D1 DE8080900330T DE3065491T DE3065491D1 DE 3065491 D1 DE3065491 D1 DE 3065491D1 DE 8080900330 T DE8080900330 T DE 8080900330T DE 3065491 T DE3065491 T DE 3065491T DE 3065491 D1 DE3065491 D1 DE 3065491D1
Authority
DE
Germany
Prior art keywords
pilot
stick
term
desensitizing
inadvertent
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
Application number
DE8080900330T
Other languages
English (en)
Inventor
Don L Adams
Richard D Murphy
William C Fischer
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 DE3065491D1 publication Critical patent/DE3065491D1/de
Expired legal-status Critical Current

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)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Toys (AREA)
  • Catching Or Destruction (AREA)
  • Feedback Control In General (AREA)
  • Selective Calling Equipment (AREA)
  • Traffic Control Systems (AREA)
  • Mechanical Control Devices (AREA)
DE8080900330T 1979-01-24 1980-01-16 Desensitizing helicopter control response to inadvertent pilot input Expired DE3065491D1 (en)

Applications Claiming Priority (2)

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
PCT/US1980/000035 WO1980001557A1 (en) 1979-01-24 1980-01-16 Desensitizing helicopter control response to in advertent pilot input

Publications (1)

Publication Number Publication Date
DE3065491D1 true DE3065491D1 (en) 1983-12-15

Family

ID=21720289

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8080900330T Expired DE3065491D1 (en) 1979-01-24 1980-01-16 Desensitizing helicopter control response to inadvertent pilot input

Country Status (11)

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

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4387431A (en) * 1981-03-30 1983-06-07 United Technologies Corporation Roll attitude inhibit of aircraft automatic outer loop
US4387432A (en) * 1981-03-30 1983-06-07 United Technologies Corporation Pulsed aircraft actuator
US4387430A (en) * 1981-03-30 1983-06-07 United Technologies Corporation Pitch stick force inhibit of aircraft automatic outer loop
US4417308A (en) * 1981-03-30 1983-11-22 United Technologies Corporation Dual inner loop fault inhibit of aircraft outer loop
US4385355A (en) * 1981-03-30 1983-05-24 United Technologies Corporation Automatic outer loop centering of aircraft inner 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
US9150308B2 (en) 2012-02-10 2015-10-06 Merlin Technology, Inc. Rotorcraft autopilot system, components and methods
WO2013120031A1 (en) 2012-02-10 2013-08-15 Merlin Technology, Inc. Autopilot control arrangement 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
DK146588C (da) 1984-04-30
EP0022847A1 (de) 1981-01-28
EP0022847B1 (de) 1983-11-09
DK146588B (da) 1983-11-14
NO146947C (no) 1983-01-05
NO802804L (no) 1980-09-23
WO1980001557A1 (en) 1980-08-07
NO146947B (no) 1982-09-27
EP0022847A4 (de) 1981-07-16
JPH01116000U (de) 1989-08-04
CA1127133A (en) 1982-07-06
AU5484880A (en) 1980-07-31
IL59194A (en) 1984-01-31
US4279391A (en) 1981-07-21
ATE5245T1 (de) 1983-11-15
AU529394B2 (en) 1983-06-02
DK385780A (da) 1980-09-11
JPS56501445A (de) 1981-10-08

Similar Documents

Publication Publication Date Title
DE3065491D1 (en) Desensitizing helicopter control response to inadvertent pilot input
DE3762027D1 (de) Fluegelklappensteuersystem eines flugzeuges.
GB2073114B (en) Multi-axis force stick self-trimmed aircraft flight control system
DK272485A (da) Fremgangsmaade til eftersoegning af personer eller genstande, f.eks. paa havet, og helikopter til udoevelse af fremgangsmaaden
JPS53109397A (en) Perceiving device for force of flight control for aeroplane
DE3366195D1 (en) Declutching control stick for an aircraft copilot
SE8400953D0 (sv) Manoverkraftgradientsystem
BR8400673A (pt) Sistema para controlar a arfada de um aviao durante operacoes de decolagem e de voo em circulos
GB2136604B (en) Helicopter attitude and airspeed acquisition and retention system
GB803574A (en) Control systems for aircraft
JPS5277399A (en) Automatic flight control system for rotary-wing aircraft
CALDWELL et al. Effect of hysteresis on the performance of a highly augmented flight control system
Gibson Flying qualities and the fly-by-wire aeroplane
FR1269506A (fr) Système automatique de commande notamment pilote automatique d'avion
JIANPEI et al. Open loop optimal control of multi-engine aircraft after one engine failure
HARRINGTON The optimal control frequency response problem in manual control(of manned aircraft systems)
Sensburg et al. Active flutter suppression on an F-4 F aircraft with external stores using already existing control surfaces
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)
Smith Input/output coupling in eigenstructure assignment
PUCK Stressed-skin construction of glider components using glass fiber plastics
OBERMAYER et al. Techniques in the assessment of helicopter flying qualities
KUBBAT Evaluation of a digital helicopter control system(BO-105 helicopter)
MOORHOUSE et al. The STOL and maneuver technology program integrated control system[Abstract Only]
COTTON Three-axis fluidic/electronic automatic flight control system flight test report[Final Report, 1 Jun. 1973- 25 Jan. 1974]
JPS56143014A (en) Inducing device of flying body

Legal Events

Date Code Title Description
8339 Ceased/non-payment of the annual fee