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특허 상세정보

Process for piloting and guiding projectiles in the terminal phase and a projectile comprising means for implementing th

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F41G-007/20    F42B-015/02   
미국특허분류(USC) 244/322 ; 244/316
출원번호 US-0204039 (1980-11-04)
우선권정보 FR-0027712 (1979-11-09)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 37  인용 특허 : 2
초록

A process for piloting and guiding a projectile in the terminal phase in which the correction is obtained by means of a barrel of (n) impellers

대표
청구항

A method for correcting the terminal portion of the ballistic trajectory of a rotating projectile directed toward a target; said projectile having a barrel of impeller each provided with at least one lateral nozzle equally spaced around the circumference of the projectile body and an optical sensor located within the nose section, said method comprising the steps of: (a) measuring the period of rotation T of the projectile about its longitudinal axis (A-B); (b) detecting the optical image (C1) of the target (C) on the successive rotations of the projecti...

이 특허를 인용한 특허 피인용횟수: 37

  1. Hultman, John A.. Adjustable range munition. USP2013128618455.
  2. Morgan, Robert W; Borg, Eric J; Leal, Michael A; Nicholl, Adam D. Air vehicle with bilateral steering thrusters. USP2015069068808.
  3. Stessen Lothar (Lauf/Pegnitz DEX). Ammunition article controllable during its final flight phase and method for navigation thereof towards a target. USP1987064674408.
  4. Roucoux Bertrand (Saint Jean le Blanc FRX). Control of a projectile by multi-chamber and single-nozzle impeller. USP1997085657948.
  5. Deffayet Jean (Chaville FRX). Device designed to modify the trajectory of a projectile by pyrotechnical thrusters. USP1991095044156.
  6. O'Dwyer, James Michael. Directional control of missiles. USP2005056889935.
  7. Horwath, Tibor G.. Guidance seeker system with optically triggered diverter elements. USP2004076766979.
  8. Horwath, Tibor G.. Guidance seeker system with optically triggered diverter elements. USP2004116817569.
  9. Linick, James M.. Impulse motor and apparatus to improve trajectory correctable munitions including cannon launched munitions, glide bombs, missiles, rockets and the like. USP2004046722609.
  10. Stessen Lothar (Lauf DEX). Impulse propulsion unit. USP1987094689845.
  11. Arthur J. Schneider ; James G. Small. Impulse radar guidance apparatus and method for use with guided projectiles. USP2002096450442.
  12. Strassman, Doron; Elkanick, Mark E.. Integrated propulsion and attitude control system from a common pressure vessel for an interceptor. USP2015038975565.
  13. Goldberg, Marshall Phillip. Laser-guided projectile system. USP2016039279651.
  14. John, Lawrence E.. Low mass flow reaction jet. USP2004066752351.
  15. Rodden, John J.; Turner, Andrew E.. Method and system for synchronized forward and Aft thrust vector control. USP2004026695251.
  16. Seidensticker, Jens. Method for correcting the trajectory of a projectile, in particular of a terminal phase-guided projectile, and projectile for carrying out the method. USP2013108558151.
  17. Kinsey, Jr., Lloyd E.; Cook, James M.. Method of controlling missile flight using attitude control thrusters. USP2011118058596.
  18. Blackburn, Thomas R.. Methods and apparatus for guiding a projectile. USP2011017872215.
  19. 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.
  20. Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin. Methods and apparatuses for aerial interception of aerial threats. USP2017019551552.
  21. Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin. Methods and apparatuses for engagement management of aerial threats. USP20190310228689.
  22. Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin. Methods and apparatuses for engagement management of aerial threats. USP2016119501055.
  23. Geis Norman P. (Kensington NH) Chambers Edward A. (Acton MA). Mortar system with improved round. USP1985084533094.
  24. Biggers James E. ; Finn Kevin P. ; Schwartz ; II Homer H.. Neural network controller for a pulsed rocket motor tactical missile system. USP2000106138945.
  25. Eric Larcher FR; Cyril Delmau FR. Process and device for guiding a flying craft, in particular a missile, onto a target. USP2002036360986.
  26. Romer Rudolf,DEX ; Wollmann Gerd,DEX. Projectile having an apparatus for flight-path correction. USP1998115836540.
  27. 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.
  28. 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.
  29. Horwath Tibor G.. Reticle for use in a guidance seeker for a spinning projectile. USP2000066076765.
  30. Tibor G. Horwath. Reticle for use in a guidance seeker for a spinning projectile. USP2002036357695.
  31. Facciano, Andrew B.; Graves, William G.; Barker, Michael A.; Alkema, Michael S.; Larson, Jeffrey S.. Rocket cluster divert and attitude control system. USP2016069377279.
  32. Crawford, James I.; Howell, W. Max. Spin stabilized impulsively controlled missile (SSICM). USP1985124560120.
  33. 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.
  34. 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.
  35. Palathingal, Mohan J.; Grau, John C.. Technique for improving accuracy of high speed projectiles. USP2003056565036.
  36. Metz Pierre (Paris FRX). Terminal guidance method and a guided missile operating according to this method. USP1986024568040.
  37. Bittle,David A.; Jimmerson,Gary T.; Cothran,Julian L.. Trajectory correction kit. USP2008087416154.