$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Total energy based flight control system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-013/00   
미국특허분류(USC) 364/434; 364/440; 244/181; 244/182
출원번호 US-0454205 (1982-09-30)
국제출원번호 PCT/US82/01388 (1982-09-30)
§371/§102 date [Act 371]19820930 ([Act 101]19820930)
국제공개번호 WO84/01345 (1984-04-12)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Hamley, James P.Donahue, Bernard A.
인용정보 피인용 횟수 : 50  인용 특허 : 7
초록

An integrated aircraft longitudinal flight control system uses a generalized thrust and elevator command computation (38), which accepts flight path angle, longitudinal acceleration command signals, along with associated feedback signals, to form energy rate error (20) and energy rate distribution error (18) signals. The engine thrust command is developed (22) as a function of the energy rate distribution error and the elevator position command is developed (26) as a function of the energy distribution error. For any vertical flight path and speed mode t...

대표
청구항

1. An aircraft longitudinal flight control system for automatically controlling the aircraft's flight path and speed, using engine thrust and elevator control surface position, comprising: means for developing an incremental net thrust command signal ΔT c which is a linear combination of a signal representative of the aircraft's total energy error with respect to the flight path and speed command targets and a signal representative of the rate of change of the aircraft's total energy; thrust control means for automatically controlling the incremental...

이 특허를 인용한 특허 피인용횟수: 50

  1. Lavretsky, Eugene; Hovakimyan, Naira. Adaptive control in the presence of input constraints. USP2009097593793.
  2. Ogden, Collin D.; Mickelson, Bradley R.; Kolek, Kirk A.. Aircraft energy indicator generating system, device, and method. USP2017119815571.
  3. Momenthy Albert M. (Kent WA). Aircraft energy loading method and apparatus. USP1989024809174.
  4. Partel, Walter V.. Aircraft energy systems management method. USP2003106636786.
  5. Fucke, Lars. Aircraft speed guidance display. USP2017119815567.
  6. Greene, Randall A.; Beyer, Shawn P.; Teter, Robert D.. Aircraft turbulence detection. USP2017079701422.
  7. Kelly Brian D. (Redmond WA) Pelton Scott L. (Renton WA). Apparatus and method for displaying aircraft flight path angle on an attitude display indicator. USP1991035003305.
  8. Appleford Lyle R. (Seattle WA). Apparatus and methods for generating aircraft control commands using nonlinear feedback gain. USP1989084862372.
  9. Boorman, Daniel J.; Gunn, Peter D.; Griffin, III, John C.. Apparatuses and methods for displaying autoflight information. USP2013078494691.
  10. Boorman, Daniel J.; Gunn, Peter D.; Griffin, III, John C.. Apparatuses and systems for controlling autoflight systems. USP2011067970502.
  11. Glover,John H.. Approach monitoring and advisory system and method. USP2006117132960.
  12. Nichols,William Mark; Houchard,Jack. Automatic contingency generator. USP2009037512462.
  13. Greene, Randall A.; Beyer, Shawn P.. Autothrottle retard control. USP2016059346552.
  14. Gillett, Luke Dafydd; Worsham, II, Robert Earl. Combined airspeed and inertial data for rotorcraft longitudinal control. USP20181010101749.
  15. Yamasaki, Koichi. Control system of aircraft, method for controlling aircraft, and aircraft. USP2015069045220.
  16. Calandra, Salvatore; Morgan, Keith. Cruise control FADEC logic. USP2010087774106.
  17. Greene, Randall A.; Beyer, Shawn P.. Deflare pitch command. USP2017019546003.
  18. Barral, Jérôme; Lopez, Salvador; Gerard, Eric. Device for displaying the energy variation of an aircraft, corresponding method and system for displaying the energy variation. USP2014048706324.
  19. Sherry, Lance C.; Quarry, Steven T.. Display of altitude and path capture trajectories. USP2005036870490.
  20. Clark, Samuel T.; Johnson, Keith L.; Neff, Andrew D.; Bowe, Roglenda R.. Display of taxi route control point information. USP2013028386167.
  21. Thornberg Christopher A. ; Cotton Bryan S.. Earth-referenced wind adjustment for hovering aircraft. USP2000066076024.
  22. Burken John J. ; Burcham ; Jr. Frank W.. Emergency control aircraft system using thrust modulation. USP2000036041273.
  23. Patera, Russell Paul. Energy-angular momentum diagnostic method for launch vehicle performance. USP2014038676407.
  24. Hackelman Kris L. (Mukilteo WA) Kontvis Alfons R. (Alderwood Manor WA). Engine trim tachometer unit and calibration method. USP1990044918629.
  25. Greene, Leonard M.. Flare control system. USP2004016676088.
  26. Andre, Joan; Joye, Jacky; Malagoli, Armand; Moulis, Fran?ois. Flight control indicator for an aircraft, in particular a transport airplane, intended to supply the thrust generated by at least one engine of the aircraft. USP2005066904340.
  27. Zweifel Terry L. (Phoenix AZ) Johnson David A. (Chandler AZ). Flight guidance system for aircraft in windshear. USP1989014797674.
  28. Garrido-Lopez, David; Gomez Ledesma, Ramon. Four-dimensional guidance of an aircraft. USP2014038676403.
  29. Gomez Ledesma, Ramon; Garrido-Lopez, David; D'Alto, Luis Pedro. Four-dimensional navigation of an aircraft. USP2017109785153.
  30. Sauer Douglass J.. Fuel time indicator. USP1998065760712.
  31. Lemaignan, Benoît; Mathieu, Gérard. Method and device for controlling the thrust of a multi-engine aircraft. USP2013018359129.
  32. DeMers, Robert E.; Meyers, David W.; Buchanan, Brian R.; Spoor, David T.. Method and system for context sensitive aircraft navigation. USP2010067742847.
  33. Lacoste, Jean-Patrick; Boubal, Jean-Jacques; Dupont De Dinechin, Sébastien. Method and system for managing the energy variation of an aircraft. USP2013098527173.
  34. Klooster, Joel Kenneth. Method and system for vertical navigation using time-of-arrival control. USP2012118321071.
  35. Nolte Edward P. ; Myers Michael J. ; Coombs David C. ; Griffin ; III John C.. Method of automated thrust-based roll guidance limiting. USP2001086282466.
  36. Vos, David W.. Method, apparatus and design procedure for controlling multi-input, multi-output (MIMO) parameter dependent systems using feedback LTI'zation. USP2005026859689.
  37. Vos, David W.. Method, apparatus and design procedure for controlling multi-input, multi-output (MIMO) parameter dependent systems using feedback LTI'zation. USP2003036539290.
  38. Clark, Aidan William; Ortlepp, Hans Max. Methods and systems for jet engine overthrust protection. USP2003066578794.
  39. Halladay, Henry E.; Edewaard, David O.; Swann, Terry M.. Remote programmable reference. USP2012128331888.
  40. 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. USP2012078214089.
  41. Clark, Samuel T.; Bowe, Roglenda R.; Jones, Wayne R.. System and method for taxi route entry parsing. USP2012058180562.
  42. Zweifel, Terry L.. Systems and methods for aircraft windshear detection. USP2013088508387.
  43. Boorman, Daniel J.; Bresley, William M.; Griffin, III, John C.; Gunn, Peter D.; Mumaw, Randall J.. Systems and methods for presenting and obtaining flight control information. USP2013088504223.
  44. Greene, Randall A.. Systems and methods for safely landing an aircraft. USP2015069051061.
  45. Eggold, David P.; Flanzer, Tristan C.. Systems and methods to prevent an aircraft from tail contact with the ground. USP2018069989972.
  46. Greene, Randall A.; Beyer, Shawn. Tailstrike warning system. USP2017119828113.
  47. William Michael Hopkins ; Samuel Patrick Landers ; Stephen F Roth. Tire initiated vehicle control system. USP2002126498967.
  48. Lambregts Antonius A.. Total energy based flight control system. USP2000056062513.
  49. Shepler, Angela J.. Turbine engine thrust scheduling. USP2014038682562.
  50. Zweifel Terry L. (Phoenix AZ). Windshear guidance for aircraft having inertial sensor. USP1990014893245.