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"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Method of determining and controlling the attitude of a spin-stabilized satellite in an elliptical transfer orbit

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/24   
미국특허분류(USC) 244/164 ; 244/169 ; 364/434
출원번호 US-0446254 (1989-12-05)
우선권정보 FR-0017120 (1988-12-23)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 10  인용 특허 : 0
초록

The attitude of a satellite carrying terrestrial and solar sensors and spin-stabilized about an axis V-V is determined and controlled prior to its transfer from an elliptical transfer orbit to a circular geostationary orbit by means of an apogee motor firing. The attitude is defined relative to an inertial X-Y-Z frame of reference the Z axis of which is directed towards geographical North, by a declination abba

대표
청구항

Method of determining and controlling the attitude of a satellite carrying terrestrial and solar sensors and spin-stabilized about an axis V-V prior to its transfer from an elliptical transfer orbit to a circular geostationary orbit by means of an apogee motor firing, said attitude being defined relative to an inertial X-Y-Z frame of reference the Z axis of which is directed towards geographical North, by a declination abb10°from the apogee of said transfer orbit, the declination a

이 특허를 인용한 특허 피인용횟수: 10

  1. Belbruno Edward A.. Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same. USP2001066253124.
  2. Belbruno Edward A.. Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same. USP2000086097997.
  3. Belbruno, Edward A.. Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same. USP2004066751531.
  4. Belbruno, Edward A.. Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same. USP2003066577930.
  5. Belbruno,Edward A.. Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same. USP2006026999860.
  6. Edward A. Belbruno. Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same. USP2002016341250.
  7. Peck,Mason A.. Momentum stabilized launch vehicle upper stage. USP2006087090171.
  8. Edward A. Belbruno. Procedure for generating operational ballistic capture transfer using a computer implemented process. USP2002086442482.
  9. Belbruno Edward A.. Procedure for generating operational ballistic capture transfer using computer implemented process. USP2001086278946.
  10. Edward A. Belbruno. System and method of a ballistic capture transfer to L4, L5. USP2002056385512.