$\require{mediawiki-texvc}$
  • 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"

특허 상세정보

Attitude control device using solar sails for a satellite stabilized on three axes

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/44   
미국특허분류(USC) 244/173 ; 244/168 ; 136/244
출원번호 US-0632455 (1990-12-21)
우선권정보 FR-0017479 (1989-12-29)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 15  인용 특허 : 0
초록

An attitude control device for a satellite stabilized on three axes including a pitch axis comprises two solar generator wings extending in opposite directions away from a satellite body on respective longitudinal axes at least approximately parallel to the pitch axis. Two drive motors drive these wings independently of each other in rotation about rotation axes at least approximately parallel to the pitch axis to keep the wings facing the Sun with a depointing angle at most equal to a predetermined maximum depointing value. Sensors measure attitude angl...

대표
청구항

Attitude control device for a satellite stabilized on three axes including a pitch axis, the device comprising two solar generator wings extending in opposite directions away from a satellite body on opposite respective wing longitudinal axes at least approximately parallel to the pitch axis, two drive motors adapted to drive said wings independently of each other in rotation about respective rotation axes at least approximately parallel to the pitch axis to keep said wings facing the Sun with a depointing angle at most equal to a predetermined maximum w...

이 특허를 인용한 특허 피인용횟수: 15

  1. William A. Hoskins ; Robert J. Cassady. ARC discharge initiation for a pulsed plasma thruster. USP2002046373023.
  2. Basuthakur Sibnath ; Bonello David Paul ; Allen Robert David. Actively controlled thermal panel and method therefor. USP1999126003817.
  3. Draim John E.. Adaptively positioned solar array. USP2001056227497.
  4. Reutenauer, Xavier; Samson, Philippe. Articulated assembly of solar generator panels and space vehicle. USP2009047513461.
  5. Price Xen ; Chan Kam. Autonomous solar torque management. USP1999125996942.
  6. Lagadec, Kristen; Chabot, Thomas. Device for monitoring the attitude of a satellite, and method for controlling a satellite provided with said device. USP2016019227740.
  7. 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.
  8. Polle, Bernard. Method of controlling the attitude of a satellite and an attitude-controlled satellite. USP2015059027887.
  9. Basuthakur Sibnath ; Ibanez-Meier Rodrigo ; Stratman Bob Dennis. Multiple axis solar sailing. USP1999055906339.
  10. Whorton, Mark Stephen; Redmon, Jr., John W.; Cox, Mark D.. Orientation control method and system for object in motion. USP2012018090484.
  11. Cande Jacques,NLX. Passive device for stabilizing the direction in which a spacecraft points. USP2000086102336.
  12. Wehner, James; Rudd, Lael; Harris, Christian; Foroozan, Shahram. Solar array momentum control. USP2011077980514.
  13. Shah Piyush R. ; Bender Douglas J.. Spacecraft acquisition of sun pointing. USP2000026019320.
  14. Goodzeit,Neil E.; Ratan,Santosh. Spacecraft disturbance trimming system. USP2006097104506.
  15. Munir, Mohammad Saghir; Cooper, John Hutton; Hirschberg, Philip Conway. Spacecraft momentum management using solar array. USP2014108868263.