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특허 상세정보

Trajectory correction kit

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F41G-007/00    F42B-015/01    F42B-015/00   
미국특허분류(USC) 244/003.22; 244/003.1; 244/003.15; 244/003.21
출원번호 US-0229425 (2005-09-16)
등록번호 US-7416154 (2008-08-26)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Chang,Hay Kyung
인용정보 피인용 횟수 : 16  인용 특허 : 28
초록

The Trajectory Correction Kit (TCK) is a completely self-contained retrofit kit that is externally and fixedly mounted as an add-on to the rear (aft of the tailfins) of an existing, unguided rocket. The TCK continuously measures the pitch and yaw of the rocket as it is released from the launch tube and during the initial seconds of the flight and calculates the trajectory correction that is necessary to eliminate the measured pitch and yaw. Then it activates selected thrusters among the thrusters that are positioned around the circumference of the rocke...

대표
청구항

We claim: 1. A trajectory correction kit (TCK) to neutralize the perturbations in the trajectory of a rocket upon launch so as to enable the rocket to impact on a pre-selected target more accurately, said correction kit being externally mounted on the rocket, between the tailfins and the end of the body of the rocket, and comprising: a plurality of thrusters, said thrusters being deployed around the circumference of the rocket; a control computer coupled to said thrusters, said computer activating particular thrusters from time to time to effect pre-cal...

이 특허에 인용된 특허 (28)

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  2. Peoples John R. (Moorpark CA) Phillips Billy R. (Canoga Park CA). Detachable thrust vector mechanism for an aeronautical vehicle. USP1989074844380.
  3. Schwarzkopf Gerhart (Uhldingen-Mhlhofen DEX) Dulat Bernd (Uberlingen/Bodensee DEX). Device for measuring the roll rate or roll attitude of a missile. USP1988124790493.
  4. O'Dwyer, James Michael. Directional control of missiles. USP2005056889935.
  5. Metz Pierre (Paris FRX). Gas jet steering device and method missile comprising such a device. USP1984084463921.
  6. Stessen Lothar (Lauf DEX). Impulse propulsion unit. USP1987094689845.
  7. Grau, John C.; Fiorellini, Arthur J.; Carr, Raymond E.. Jump correcting projectile system. USP2003106629668.
  8. Bagley Cloy J. (Fountain Valley CA). Lateral thrust assembly for missiles. USP1992075129604.
  9. Heitmann,Thomas; Schwenzer,Michael. Lateral thrust control. USP2006107118065.
  10. John, Lawrence E.. Low mass flow reaction jet. USP2004066752351.
  11. Nelson Steven D. ; Sipes William J. ; Hoffmaster David K.. Mems synthesized divert propulsion system. USP2001016178741.
  12. Rodden, John J.; Turner, Andrew E.. Method and system for synchronized forward and Aft thrust vector control. USP2004026695251.
  13. Schfer Berthold (Bergisch Gladbach DEX). Missile. USP1987124712748.
  14. Morris Joseph W. (Rancho Cordova CA) Carlson Russell W. (Folsom CA) Peterson Kevin L. (Sacramento CA) Reich Edward M. (Orangevale CA). Multiple pintle nozzle propulsion control system. USP1995105456425.
  15. Mayersak Joseph R.. Precision guidance system for aircraft launched bombs. USP2001076254031.
  16. Mayersak Joseph R. (Ashburn VA). Precision guidance system for aircraft launched bombs. USP1996045507452.
  17. Mayersak Joseph R. (Ashburn VA). Precision guidance system for aircraft launched bombs. USP1997085657947.
  18. Metz Pierre (Paris FRX). Process for piloting and guiding projectiles in the terminal phase and a projectile comprising means for implementing th. USP1983104408735.
  19. Folsom,Mark; Piper, III,Charles; Fahey,Wm. David; McGowan,Jared M.. Projectile diverter. USP2006027004423.
  20. Mark Folsom ; Charles Piper, III ; Wm. David Fahey ; Jared M. McGowan. Projectile diverter. USP2002046367735.
  21. Bar Klaus (Lauf DEX) Lehrieder Gunther (Rothenbach DEX). Projectile with correctable trajectory. USP1991105054712.
  22. Sturm Richard (Ottobrunn DEX). Remote control system for a rolling flying body. USP1990054928906.
  23. Waymeyer Walter K. (LaVerne CA) Banach Timothy P. (Chino CA). Roll damper for thrust vector controlled missile. USP1993115259569.
  24. 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.
  25. Thomas E. Harkins ; T. Gordon Brown. System and method for reducing dispersion of small rockets. USP2002026347763.
  26. Morgand Jean-Pierre (Paris FRX). System for steering a missile by means of lateral gas jets. USP1992065123611.
  27. Smith Gregory H. ; Clark Roland D.. Universal driver circuit for actuating both valves and ordnances. USP2001076267326.
  28. Woessner, George T.; Abel, Stephen G.; Baker, Mark H.; Alexander, Dennis M.. Vehicle, lightweight pneumatic pilot valve and related systems therefor. USP2005106951317.

이 특허를 인용한 특허 피인용횟수: 16

  1. Hultman, John A.. Adjustable range munition. USP2013128618455.
  2. Shpund, Zalman Shlomo; Sahar, David. Airborne guided shell. USP2012108278611.
  3. Green, Andrew Walter. Decoupled multiple weapon platform. USP2012088245624.
  4. Vaidya, Uday; Andrews, J. Barry; Pillay, Selvum; Ning, Haibin. Long fiber thermoplastic thin-walled baseplates for missile applications and methods of manufacture. USP2012108277933.
  5. Caye, Paul; Caillaud, James; Laporte, Guillaume. Method and system for piloting a flying craft with rear propulsion unit. USP2014098825231.
  6. Blackburn, Thomas R.. Methods and apparatus for guiding a projectile. USP2011017872215.
  7. Sharpin, David; Kolanek, Jim; Cvetnic, Mark A.; Hutchings, Mike; Tennison, James; Nelson, Kent Carl; Hunsberger, Harold Kregg; Baseghi, Behshad. Methods and apparatuses for active protection from aerial threats. USP2015109170070.
  8. Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin. Methods and apparatuses for aerial interception of aerial threats. USP2017019551552.
  9. Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin. Methods and apparatuses for engagement management of aerial threats. USP20190310228689.
  10. Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin. Methods and apparatuses for engagement management of aerial threats. USP2016119501055.
  11. Alexander, Steven B.; Redhead, Richard. Mortar round glide kit. USP2012088237096.
  12. Starken, George M.. Post boost control power assembly. USP2011017875838.
  13. Preston, Kenneth G.; Leal, Michael A.; Wilson, Rondell J.; Hussey, Richard C.. Propulsion and maneuvering system with axial thrusters and method for axial divert attitude and control. USP2014058735788.
  14. Green, Gary B.; Scherrer, Francis Keith; Doty, James H.. Rotation rate tracking system using GPS harmonic signals. USP2012098260478.
  15. 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.
  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 and application to an active protection system. USP2011087989743.