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Volumn 25, Issue 2, 2002, Pages 387-393

Hybrid Cartesian and orbit element feedback law for formation flying spacecraft

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; COMPUTER SIMULATION; ORBITS; SATELLITES; TRACKING (POSITION);

EID: 0036494036     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4893     Document Type: Article
Times cited : (100)

References (19)
  • 8
    • 85003321464 scopus 로고
    • Elliptic elements in terms of small increments of position and velocity components
    • (1963) AIAA Journal , vol.1 , Issue.9 , pp. 2626-2629
    • DeVries, J.P.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.