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FR1353123A - Helicopter automatic flight control system - Google Patents

Helicopter automatic flight control system

Info

Publication number
FR1353123A
FR1353123A FR924716A FR924716A FR1353123A FR 1353123 A FR1353123 A FR 1353123A FR 924716 A FR924716 A FR 924716A FR 924716 A FR924716 A FR 924716A FR 1353123 A FR1353123 A FR 1353123A
Authority
FR
France
Prior art keywords
control system
flight control
automatic flight
helicopter automatic
helicopter
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
FR924716A
Other languages
French (fr)
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.)
North American Aviation Corp
Original Assignee
North American Aviation 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 North American Aviation Corp filed Critical North American Aviation Corp
Priority to FR924716A priority Critical patent/FR1353123A/en
Application granted granted Critical
Publication of FR1353123A publication Critical patent/FR1353123A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • 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)
  • Mechanical Engineering (AREA)
FR924716A 1963-02-13 1963-02-13 Helicopter automatic flight control system Expired FR1353123A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR924716A FR1353123A (en) 1963-02-13 1963-02-13 Helicopter automatic flight control system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR924716A FR1353123A (en) 1963-02-13 1963-02-13 Helicopter automatic flight control system

Publications (1)

Publication Number Publication Date
FR1353123A true FR1353123A (en) 1964-02-21

Family

ID=8796994

Family Applications (1)

Application Number Title Priority Date Filing Date
FR924716A Expired FR1353123A (en) 1963-02-13 1963-02-13 Helicopter automatic flight control system

Country Status (1)

Country Link
FR (1) FR1353123A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2348104A1 (en) * 1976-04-12 1977-11-10 United Technologies Corp IMPROVEMENTS RELATING TO SYSTEMS INTENDED TO INCREASE IN-FLIGHT STABILITY OF GIRAVIONS
CN114248911A (en) * 2021-12-24 2022-03-29 兰州飞行控制有限责任公司 Helicopter electric series steering engine control signal adjusting method

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2348104A1 (en) * 1976-04-12 1977-11-10 United Technologies Corp IMPROVEMENTS RELATING TO SYSTEMS INTENDED TO INCREASE IN-FLIGHT STABILITY OF GIRAVIONS
CN114248911A (en) * 2021-12-24 2022-03-29 兰州飞行控制有限责任公司 Helicopter electric series steering engine control signal adjusting method
CN114248911B (en) * 2021-12-24 2024-03-01 兰州飞行控制有限责任公司 Helicopter electric series steering engine control signal adjustment method

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