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Stall and recovery control system 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • G06F-017/00
  • G06F-007/00
출원번호 US-0359349 (1999-07-21)
발명자 / 주소
  • Kaloust Joseph H.
출원인 / 주소
  • Lockheed Martin Corporation
대리인 / 주소
    Sidley & AustinSadacca
인용정보 피인용 횟수 : 14  인용 특허 : 25

초록

An autopilot controller, for controlling a vehicle traveling in a fluid medium, designed for controlling the vehicle in any one of pre stall, stall and post stall regions. The autopilot controller provides an approach for one-to-one mapping between a target force or moment command which is received

대표청구항

[ That which is claimed is:] [1.]1. An autopilot controller suitable for controlling a vehicle, traveling in a fluid medium, in response to a commanded maneuver, said controller being capable of controlling said vehicle in a pre-stall region, a stall region and a post-stall region, said vehicle havi

이 특허에 인용된 특허 (25)

  1. Lambregts Antonius A. (Issaquah WA), Aircraft flight path angle display system.
  2. Millen Ernest W. (Seaford VA), Aircraft liftmeter.
  3. Martorella Romeo P. (Dix Hills NY), Aircraft precision approach control system.
  4. Bala Paul F. (Issaquah WA) Kupcis Edgars A. (Redmond WA) Fisher William B. (Bellevue WA), Aircraft stall warning system.
  5. Nadkarni Arun A. (12836 NE. 135th St. Kirkland WA 98034) Sankrithi Mithra M. K. V. (4554 143rd Ave. ; SE. Bellevue WA 98006), Apparatus and methods for automatically maintaining aircraft track angle.
  6. Gast Mark E., Autopilot/flight director stall protection system.
  7. Gast Mark E., Autopilot/flight director underspeed protection system.
  8. Gast Mark E., Autopilot/flight director underspeed protection system.
  9. Burdoin Robert B. (Albuquerque NM), Canard based high angle of attack air data sensor.
  10. Vos David W., Fault tolerant automatic control system utilizing analytic redundancy.
  11. Vos David W. (Boston MA), Fault tolerant automatic control system utilizing analytic redundancy.
  12. Orgun Munir (Woodinville WA) McRoberts Timothy C. (Bothell WA) Wu Tzong-Hsiu B. (Redmond WA), Ground effects compensated real time aircraft body angle of attack estimation.
  13. Bauer Carl J. (Glassboro NJ), Ground state-fly state transition control for unique-trim aircraft flight control system.
  14. Fowler Donald W. (Oxford CT) Lappos Nicholas D. (Milford CT) Edwards Joan A. (Fairfield CT), Helicopter integrated fire and flight control having a pre-launch and post-launch maneuver director.
  15. Fowler Donald W. (Oxford CT) Lappos Nicholas D. (Milford CT) Dryfoos James B. (Wallingford PA) Keller James F. (Media PA), Helicopter integrated fire and flight control having azimuth and pitch control.
  16. Quinlivan Richard Paul (Binghamton NY), High angle of attack aircraft control system utilizing a pseudo acceleration signal for control purposes.
  17. Bateman Charles D. (Bellevue WA), Independent low airspeed alert.
  18. Gold Phillip J. (Shelton CT) Fogler ; Jr. Donald L. (Milford CT) Dryfoos James B. (Wallingford PA), Inertial velocity command system.
  19. Berwick ; Jr. James W. (Seattle WA) Bleeg Robert J. (Mercer Island WA) McFaddin Vincent E. (Renton WA), Method and apparatus for an aircraft climb-out guidance system.
  20. von Gersdorff Michael (Dietramszell DEX), Method and apparatus for trimming and stabilizing an aircraft.
  21. Palmer Steven D., Method for flight parameter monitoring and control.
  22. Pelton, Scott L., Pitch attitude command flight control system for landing flare.
  23. Brown Jerry A. (Hazelwood MO), Stall avoidance system for aircraft.
  24. Gold Phillip J. (Shelton CT) Fogler ; Jr. Donald L. (Milford CT) Richard James L. (Stratford CT), Transient free synchronizer for autopilot systems.
  25. Jackson Joseph W. (Glendale AZ), Vehicle control surface position feedback compensator for reducing vehicle oscillation.

이 특허를 인용한 특허 (14)

  1. Higuchi, Yosuke; Matsuda, Takeshi, Aircraft and aircraft control method.
  2. Prosser, Kevin, Aircraft flight envelope protection and recovery autopilot.
  3. Zyskowski,Michael Kyle, Automatic longitudinal pitch trim in aircraft combat simulation.
  4. Cherepinsky, Igor, Automatic trim system for fly-by-wire aircraft with unique trim controllers.
  5. Clark, Aidan William; Ortlepp, Hans Max, Methods and systems for jet engine overthrust protection.
  6. O'Brien, John F., Rudder roll stabilization by nonlinear dynamic compensation.
  7. Schulte, Kynn J.; Fortenbaugh, Robert L.; Builta, Kenneth E., Stall prevention/recovery system and method.
  8. Caldeira, Fabricio Reis; Gangsaas, Dagfinn; Polati de Souza, Alvaro Vito; Martins, Eduardo da Saiva; Vita, Marco Tulio Sguerra; Filho, Jose Marcio Vieira Dias; Campos, Marcos Vinicius; Freitas, Emerson, Stall, buffeting, low speed and high attitude protection system.
  9. Caldeira, Fabricio Reis; Gangsaas, Dagfinn; Polati de Souza, Alvaro Vito; Martins, Eduardo da Silva; Vita, Marco Tulio Sguerra; Filho, Jose Marcio Vieira Dias; Campos, Marcos Vinicius; Freitas, Emerson, Stall, buffeting, low speed and high attitude protection system.
  10. Hanel, Martin, System and method for converting an aircraft from a flight condition lying outside a permissible flight condition range to a flight condition lying within the permissible flight condition range.
  11. Yudintsev, Kirill; Polyakov, Alexander, System and method for simulated aircraft control through desired direction of flight.
  12. Yudintsev, Kirill; Polyakov, Alexander, System and method for simulated aircraft control through desired direction of flight.
  13. Yudintsev, Kirill; Polyakov, Alexander, System and method for simulated aircraft control through desired direction of flight.
  14. Zweifel, Terry L., Systems and methods for aircraft windshear detection.
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