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특허 상세정보

Roll damper for thrust vector controlled missile

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F41G-007/00   
미국특허분류(USC) 244/322 ; 244/321
출원번호 US-0834183 (1992-02-05)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 21  인용 특허 : 0
초록

A control system for thrust vector controlled (TVC) cruciform missiles having only pitch and yaw thrusters is disclosed wherein roll damping feedback signals are generated from bank angle data in a separate feedback loop with appropriate gain and compensation. Additional roll rate compensation is added to the missile pitch and yaw rate control subsystem by multiplying actual roll rate by pitch and yaw control deflections and inserting the resultant roll rate compensation command in the pitch and yaw rate error control loops. The addition of these two con...

대표
청구항

In a pitch and yaw rate subsystem of a thrust vector controlled (TVC) missile, a control system for damping actual roll rate solely by deflecting a pitch and yaw thrust vector nozzle, said subsystem producing pitch and yaw deflection rate commands for deflecting said thrust vector nozzle and having an inertial measurement unit (IMU) for providing signals representing actual pitch, yaw, and roll rates, said control system comprising: means for computing a bank angle from said IMU signals, said bank angle having a pitch component and a yaw component; selec...

이 특허를 인용한 특허 피인용횟수: 21

  1. Villaume, Fabrice. Active pitch control method and device for an aircraft. USP2010127853369.
  2. DiCocco, Jack; Prince, Troy; Patel, Mehul; Ng, Tsun Ming Terry. Aircraft and missile afterbody flow control device and method of controlling flow. USP2017059637223.
  3. Schroeder Wayne K.. Dual-control scheme for improved missile maneuverability. USP200108RE37331.
  4. Schroeder Wayne K.. Dual-control scheme for improved missile maneuverability. USP1998115835869.
  5. Schroeder Wayne K. (Arlington TX). Dual-control scheme for improved missle maneuverability. USP1997055631830.
  6. Weiss Haim,ILX ; Benshabat Daniel G.,ILX. Flight control of an airborne vehicle at low velocity. USP1999035875993.
  7. Grau, John C.; Fiorellini, Arthur J.; Carr, Raymond E.. Jump correcting projectile system. USP2003106629668.
  8. Schroeder Wayne K.. Method and apparatus for rapidly turning a vehicle in a fluid medium. USP2001106308911.
  9. Caye, Paul; Caillaud, James; Laporte, Guillaume. Method and system for piloting a flying craft with rear propulsion unit. USP2014098825231.
  10. Lamorlette, G?rard. Method for piloting a spinning projectile. USP2005056886774.
  11. Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin. Methods and apparatuses for aerial interception of aerial threats. USP2017019551552.
  12. Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin. Methods and apparatuses for engagement management of aerial threats. USP20190310228689.
  13. Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin. Methods and apparatuses for engagement management of aerial threats. USP2016119501055.
  14. Nash, Gregory; Willenbring, Gary; Alford, Robert L.. Projectile control systems and methods. USP2016129518807.
  15. Barker, Michael A; Smith, Dean W; Marquart, Edward J; Corrado, Joseph R. Rocket vehicle with integrated attitude control and thrust vectoring. USP2016089429105.
  16. 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.
  17. 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.
  18. Thomas E. Harkins ; T. Gordon Brown. System and method for reducing dispersion of small rockets. USP2002026347763.
  19. Bastian, Thomas W.. Systems, apparatus and methods to compensate for roll orientation variations in missile components. USP2013018350201.
  20. Teter, Roger D.; Kudlick, Dean A.; Williams, Richard M.. Three axis flap control system. USP2003016502785.
  21. Bittle,David A.; Jimmerson,Gary T.; Cothran,Julian L.. Trajectory correction kit. USP2008087416154.