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특허 상세정보

Aircraft precision approach control system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/16    G05D-001/00   
미국특허분류(USC) 244/188 ; 244/76R ; 244/183 ; 364/428
출원번호 US-0347486 (1989-05-04)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 20  인용 특허 : 6

A precision approach control system designed to control the approach of an aircraft during landing to provide a more stable and easier mode of landing during critical landing situations, such as during the landing of an aircraft on an aircraft carrier. During operation, when the aircraft is subjected to vertical or horizontal winds or wind shear, the system controls the aircraft to maintain the inertial flight path angle constant which essentially defines operation in the precision approach control mode. In one disclosed embodiment, the precision approac...


A precision approach control system for an aircraft during landing, comprising: a said aircraft having a plurality of operating control surfaces thereon; b. on-board strap down inertial sensors on the aircraft for generating or allowing the derivation of flight path parameter information required by the precision approach control system, including a measurement of V the velocity vector of the aircraft, a measurement of NZ the acceleration of the aircraft normal to the velocity vector V of the aircraft, and a measurement of the aircraft flight path angle ...

이 특허를 인용한 특허 피인용횟수: 20

  1. Leonared M. Greene. Airborne safe landing power control system and method. USP2002096450456.
  2. Elgersma, Michael Ray; Li, Xiaohong Linda. Aircraft precision approach and shipboard landing control system and method. USP2017019547991.
  3. DeVlieg Garrett H. ; Mackness Robert F. ; Yamamoto David T.. Aircraft stop-to-position autobrake control system. USP1999105968106.
  4. Martin Mack L. ; Baciak Mark G. ; Seiler Louis W.. Banked flight stall warning device and method. USP2001016169496.
  5. Parks, Robert. Ducted spinner for engine cooling. USP2009077559191.
  6. Malta, Dan. Dynamic limitation of monoblock flight control surfaces inclinations during stall susceptibility conditions. USP2015028958930.
  7. Burcham ; Jr. Frank W. ; Burken John J. ; Le Jeanette. Emergency flight control system using one engine and fuel transfer. USP2000106126111.
  8. Kaloust Joseph H.. Enhanced stall and recovery control system. USP2001066246929.
  9. Parks,Robert. Inbound transition control for a tail-sitting vertical take off and landing aircraft. USP2009037506837.
  10. Nield Brian N. ; Landes Ross A. ; Evans Monte R.. Landing attitude modifier for airplane. USP1998105823479.
  11. Kahler Jeffrey. Lead compensated engines-only flight control system. USP2001036196499.
  12. Hiltner,Dale W.; Lee,Brian P.. Methods and systems for analyzing system operator coupling susceptibility. USP2007097272473.
  13. Kaloust Joseph H.. Stall and recovery control system. USP2001056236914.
  14. Colclough, John C.. Synthetic instrument landing system. USP2012078234021.
  15. Beaufrere, Henry L.. System and method for configuring a direct lift control system of a vehicle. USP2016089415860.
  16. Beaufrere, Henry Llewellyn. System and method for configuring a direct lift control system of a vehicle. USP2014048712606.
  17. Parks,Robert. System and method for controlling a roll rate of a torsionally-disconnected freewing aircraft. USP2008107441724.
  18. Parks,Robert; Led��,Jean Charles; Drela,Mark. System and method for controlling engine RPM of a ducted fan aircraft. USP2008047364115.
  19. Lambregts Antonius A.. Total energy based flight control system. USP2000056062513.
  20. Parks, Robert; Ledé, Jean-Charles. Vibration isolation engine mount system and method for ducted fans. USP2011088001764.