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Method and system for synchronized forward and Aft thrust vector control

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/02    F42B-015/01   
미국특허분류(USC) 244/003.21; 244/003.1; 244/003.15; 244/164; 244/169
출원번호 US-0883622 (2001-06-19)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Perman & Green, LLP
인용정보 피인용 횟수 : 10  인용 특허 : 10
초록

A system for controlling attitude about pitch, yaw, and roll axes and axial thrust of a body. The system comprises a main thrust generator located on an aft portion of the body and at least one reaction control system (RCS) located on a forward portion of the body. A thrust vector controller (TVC) is connectable to the main thrust generator and at least one RCS controller is connectable to the RCS. The RCS controller and the TVC are synchronized to adjust the direction of the principal line of thrust through the body center of gravity.

대표
청구항
▼

A system for controlling attitude about pitch, yaw, and roll axes and axial thrust of a body. The system comprises a main thrust generator located on an aft portion of the body and at least one reaction control system (RCS) located on a forward portion of the body. A thrust vector controller (TVC) is connectable to the main thrust generator and at least one RCS controller is connectable to the RCS. The RCS controller and the TVC are synchronized to adjust the direction of the principal line of thrust through the body center of gravity. one to assure that...

이 특허에 인용된 특허 (10)

  1. Roucoux Bertrand (Saint Jean le Blanc FRX). Control of a projectile by multi-chamber and single-nozzle impeller. USP1997085657948.
  2. Schroeder Wayne K.. Dual-control scheme for improved missile maneuverability. USP200108RE37331.
  3. Schroeder Wayne K. (Arlington TX). Dual-control scheme for improved missle maneuverability. USP1997055631830.
  4. Metz Pierre (Paris FRX). Process for piloting and guiding projectiles in the terminal phase and a projectile comprising means for implementing th. USP1983104408735.
  5. Bar Klaus (Lauf DEX) Lehrieder Gunther (Rothenbach DEX). Projectile with correctable trajectory. USP1991105054712.
  6. Anderson ; Jr. Carl W. (7914 Springfield Village Dr. Springfield VA 22152). Radial bleed total thrust control apparatus and method for a rocket propelled missile. USP1991075028014.
  7. Sturm Richard (Ottobrunn DEX). Remote control system for a rolling flying body. USP1990054928906.
  8. Goddard Charles W. (San Jose CA) Lucas John T. (Los Altos CA) Galvan Paul A. (San Jose CA). Solid-propellant-powered maneuvering system for spacecraft. USP1991115062593.
  9. Thomas E. Harkins ; T. Gordon Brown. System and method for reducing dispersion of small rockets. USP2002026347763.
  10. Mayersak Joseph R. (Ashburn VA). Thrust maneuver system. USP1995105456429.

이 특허를 인용한 특허 피인용횟수: 10

  1. Villaume, Fabrice. Active pitch control method and device for an aircraft. USP2010127853369.
  2. Prince, Troy S; Kolacinski, Richard; Patel, Mehul. Hierarchical closed-loop flow control system for aircraft, missiles and munitions. USP20181110139209.
  3. Turner, Andrew E.; Hart, III, William G.. Low cost launch vehicle fairing. USP20190210214303.
  4. Hamamatsu, Masanori; Kohno, Yukinobu; Higashi, Masaaki; Nakashima, Kenichi; Saito, Yasuo; Ohnishi, Hiroshi. Method and device for allocating thrust. USP2005096941195.
  5. Hamamatsu,Masanori; Kohno,Yukinobu; Higashi,Masaaki; Nakashima,Kenichi; Saito,Yasuo; Ohnishi,Hiroshi. Method and device for allocating thrust. USP2006027006905.
  6. Blackburn, Thomas R.. Methods and apparatus for guiding a projectile. USP2011017872215.
  7. Green, Gary B.; Scherrer, Francis Keith; Doty, James H.. Rotation rate tracking system using GPS harmonic signals. USP2012098260478.
  8. Brinkerhoff, Robert S.; Mahnken, Michael J.; Loehr, Richard D.; Cook, James M. System and method for attitude control of a flight vehicle using pitch-over thrusters. USP2010127851732.
  9. Brinkerhoff, Robert S.; Mahnken, Michael J.; Loehr, Richard D.; Cook, James M.. System and method for attitude control of a flight vehicle using pitch-over thrusters and application to an active protection system. USP2011087989743.
  10. Bittle,David A.; Jimmerson,Gary T.; Cothran,Julian L.. Trajectory correction kit. USP2008087416154.

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