$\require{mediawiki-texvc}$
  • 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

Method and device for electric satellite propulsion

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/00    B64G-001/24    B64G-001/40    F03H-001/00   
출원번호 US-0913975 (2014-08-29)
등록번호 US-9650159 (2017-05-16)
우선권정보 FR-13 02017 (2013-08-30)
국제출원번호 PCT/EP2014/068343 (2014-08-29)
국제공개번호 WO2015/028588 (2015-03-05)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Baker & Hostetler LLP
인용정보 피인용 횟수 : 1  인용 특허 : 17
초록

An electric propulsion device for a satellite equipped with at least four active thrusters exerting a parallel thrust upon a transfer, the device comprises means for detecting a thruster failure and means for reorienting the thrusters, and comprises means for computing a reorientation angle of the thrusters remaining active upon a failure of a thruster, the value of the angle being computed to reorient at least two of the remaining thrusters in order to cancel the total torque about the center of mass of the satellite.

대표
청구항
▼

1. A propulsion device for a satellite equipped with at least four active thrusters used in parallel, exerting a parallel thrust upon a transfer, the device comprising means for detecting a thruster failure and means for reorienting the thrusters, the device further comprising means for computing a reorientation angle of the thrusters remaining active upon a failure of a thruster, said reorientation angle being computed to reorient at least two of the remaining active thrusters according to a same computed reorientation angle in order to cancel the total...

이 특허에 인용된 특허 (17)

  1. Batla, Fawwad M.; Ho, Yiu-Hung M.. Compound steering law for efficient low thrust transfer orbit trajectory. USP2013068457810.
  2. Randolph, Thomas; Oh, David; Guenter, Fischer. Energy managed electric propulsion methods and systems for stationkeeping satellites. USP2003066581880.
  3. Batla, Fawwad M.; Ho, Yiu-hung M.. Enhanced compound steering law for general low thrust mission. USP2015018930048.
  4. Kraetz, William Francis; Karnick, Drew A.. Estimation of an initial condition inertial reference frame. USP2014038666694.
  5. Wang,Hanching Grant; Fowell,Richard A.; Ih,Che Hang C.. Method and apparatus for reaction wheel dynamic compensation in long-duration deployment of a large reflector. USP2006016990396.
  6. Douglas H. Hein ; Rongsheng Li. Method and apparatus for spacecraft payload pointing registration. USP2002086441776.
  7. Guyot, Francois. Method and system for unloading the inertia wheels of a spacecraft. USP2014088798816.
  8. Bang,Hyo Choog; Kumar,Krishna Dev; Thak,Min Jae. Method for controlling the attitude of an satellites in elliptic orbits using solar radiation pressure. USP2007037185856.
  9. Yocum ; Jr. John F. ; Cazeau Patrick A. ; Koffman Stephen J. ; Baker Douglas A.. Method of controlling attitude of a momentum biased spacecraft during long-duration thruster firings. USP2001076260805.
  10. Salvatore,Jeremiah O.; Jennings,Stephen C.; Pham,Tuan. Method of operating a satellite for end-of-life maneuvers. USP2006087093800.
  11. Stoen Jeffery D ; Chan Kam. Method to reorient a spacecraft using only initial single axis attitude knowledge. USP2000056068217.
  12. Hosick Daryl K. ; Gelon Walter S. ; Mills Richard M.. Multiple usage thruster mounting configuration. USP2000036032904.
  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. Lehner John A. (Sunnyvale CA) Holmes Thomas (Portola Valley CA). Satellite stabilization system. USP1997045618012.
  15. Sackheim Robert L. ; Bassichis James S. ; Hook Dale L.. Spacecraft attitude and velocity control thruster system. USP2000106135393.
  16. Price Xen ; Randolph Thomas ; Chan Kam K. ; Kamel Ahmed. Spacecraft attitude control system using low thrust thrusters. USP2000046053455.
  17. Eyerly, Bruce N.. Spacecraft orbit control using orbit position feedback. USP2003016508438.

이 특허를 인용한 특허 피인용횟수: 1

  1. Weiss, Avishai; Di Cairano, Stefano; Kalabic, Uros. Model Predictive control of spacecraft. USP2018019874879.

IPC 상위 출원인