$\require{mediawiki-texvc}$
  • 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"
쳇봇 이모티콘
안녕하세요!
ScienceON 챗봇입니다.
궁금한 것은 저에게 물어봐주세요.

특허 상세정보

System and method for reducing dispersion of small rockets

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/02    F42B-015/01   
미국특허분류(USC) 244/00321; 244/00315
출원번호 US-0751925 (2000-01-02)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Paul S. Clohan, Jr.
인용정보 피인용 횟수 : 20  인용 특허 : 3
초록

An active damping method and a self-contained active damping system that can be retrofitted to existing rockets are provided which for reducing the dispersion of rockets by using lateral thrusters to oppose any initial yawing motion. The self-contained system of the present invention can be installed in a cylindrical section of a rocket body by insertion between other flight body parts.

대표
청구항

1. A method for reducing dispersion of a missile launched into a trajectory toward a desired target, said launched missile having an initial yawing rate, at least one preset threshold condition for said initial yawing rate, and at least one lateral thruster, said method comprising the steps of:(a) launching the missile into said trajectory; (b) measuring the launched missile's initial yawing rate; (c) determining if said measured yawing rate exceeds said preset threshold condition; (d) selecting a lateral thruster to oppose the measured yawing rate; (e) ...

이 특허를 인용한 특허 피인용횟수: 20

  1. Morgan, Robert W; Borg, Eric J; Leal, Michael A; Nicholl, Adam D. Air vehicle with bilateral steering thrusters. USP2015069068808.
  2. O'Dwyer, James Michael. Directional control of missiles. USP2005056889935.
  3. John, Lawrence E.. Low mass flow reaction jet. USP2004066752351.
  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. Yehezkeli,Oded; Kunreich,Irad. Method and system for adjusting the flight path of an unguided projectile, with compensation for jittering deviation. USP2008127467761.
  7. Thomas E. Harkins ; David J. Hepner ; Bradford Davis. Method and system for determining magnetic attitude. USP2002126493651.
  8. Rodden, John J.; Turner, Andrew E.. Method and system for synchronized forward and Aft thrust vector control. USP2004026695251.
  9. Kinsey, Jr., Lloyd E.; Cook, James M.. Method of controlling missile flight using attitude control thrusters. USP2011118058596.
  10. 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.
  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. Dryer, Richard. Modular guided projectile. USP2013108546736.
  15. Caber,Timothy E.. Pattern classifier and method for associating tracks from different sensors. USP2007067236121.
  16. Levy, Benjamin; Goldberg, Shmuel. Reduction of rocket jet stream dispersion. USP20181010094643.
  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. USP2010127851732.
  18. 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.
  19. Teter, Roger D.; Kudlick, Dean A.; Williams, Richard M.. Three axis flap control system. USP2003016502785.
  20. Bittle,David A.; Jimmerson,Gary T.; Cothran,Julian L.. Trajectory correction kit. USP2008087416154.