$\require{mediawiki-texvc}$
  • 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"

과학기술 지식인프라 ScienceON

상세검색 다국어 입력
도움말도움말
쳇봇 이모티콘
안녕하세요!
ScienceON 챗봇입니다.
궁금한 것은 저에게 물어봐주세요.

특허 상세정보

MyON담기
내보내기

Neural network controller for a pulsed rocket motor tactical missile system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F41G-007/00   
미국특허분류(USC) 244/003.22 ; 244/164 ; 244/169 ; 102/215
출원번호 US-0004993 (1998-01-09)
발명자 / 주소
대리인 / 주소
    Collins
인용정보 피인용 횟수 : 11  인용 특허 : 9
초록
▼

A neural network controller for a pulsed rocket motor tactical missile. The missile includes a fuselage or body, with a propulsion system. The pulsed propulsion system has a need for a logical control of the application of propulsion energy throughout the missile's flight. The controller is trained to provide optimal initiation of individual rocket motor thrust pulses based on tactical information available at various points/times in the missile's flight. The controller training is through use of training cases, in which the network learns to output a sp...

대표
청구항

[ What is claimed is:] [1.] A guided missile system, comprising:a fuselage;a pulsed propulsion system comprising an N-pulse motor system for sequentially producing successive thrust pulses in response to pulse trigger commands to provide a pulsed propulsion output; andan on-board neural network controller responsive to a plurality of input condition signals for providing pulse trigger commands to control at least one of said thrust pulses at an optimal time in dependence on a set of input conditions.

이 특허에 인용된 특허 (9)

  1. Barrett Terence W. (Vienna VA). Automata networks and methods for obtaining optimized dynamically reconfigurable computational architectures and control. USP1997025602964.
  2. Jones ; Roy A. ; Mabry ; Marshall W.. Barrier system for dual-pulse rocket motor. USP1978044085584.
  3. Lincoln William P. (Simi Valley CA). Clustered neural networks. USP1992105155801.
  4. Metz Pierre (Paris FRX). Guided projectile. USP1993085238204.
  5. James Jesse C. (Huntsville AL) Blackmon ; Jr. James B. (Brownsboro AL). Hit verification technique. USP1995045406290.
  6. 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.
  7. Metz Pierre (Paris FRX). Process for piloting and guiding projectiles in the terminal phase and a projectile comprising means for implementing th. USP1983104408735.
  8. Grosgebauer Roger A. (Ogden UT) White C. Max (Brigham City UT). Radial pulse motor igniter-sustain grain. USP1991034999997.
  9. Anderson Matthew E. (China Lake CA) Menz Fredric L. (Ridgecrest CA). Safe rocket motor igniter using sequenced initiation to an explosive logic network. USP1976083973499.

이 특허를 인용한 특허 피인용횟수: 11

  1. Hultman, John A.. Adjustable range munition. USP2013128618455.
  2. Trosky, Bernhard; Wich, Harald; Lehmann, Lutz. Artillery rocket. USP2004026685134.
  3. O'Dwyer, James Michael. Directional control of missiles. USP2005056889935.
  4. Black,William L.; Marian,Steven J.. Method and apparatus for determining a position of a location dependent device. USP2008097422440.
  5. Black,William L.; Marian,Steven J.. Method and apparatus for determining a position of an attitude control motor on a guided missile. USP2008107442073.
  6. Yehezkeli,Oded; Kunreich,Irad. Method and system for adjusting the flight path of an unguided projectile, with compensation for jittering deviation. USP2008127467761.
  7. Caye, Paul; Caillaud, James; Laporte, Guillaume. Method and system for piloting a flying craft with rear propulsion unit. USP2014098825231.
  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. Palathingal, Mohan J.; Grau, John C.. Technique for improving accuracy of high speed projectiles. USP2003056565036.
  11. Brown,Charles C.; Beyer,Philip T.. Thrust vectoring a flight vehicle during homing using a multi-pulse motor. USP2006037012233.

IPC 상위 출원인