Analytical solutions for thrusting, spinning spacecraft subject to constant forces

Journal of Guidance, Control, and Dynamics

Volumn 28, Issue 6, 2005, Pages 1301-1308

  Longuski, James M ^a,d,e   Gick, R Anne ^b,f   Ayoubi, Mohammad A ^a,d   Randall, Laura ^c,f  

^a PURDUE UNIVERSITY   (United States)

^b AEROSPACE CORPORATION   (United States)

^c California Institute of Technology   (United States)

^d Purdue University   (United States)

^e AIAA   (United States)

^f M/S G19 ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; COMPUTER SIMULATION; MOTION ESTIMATION;

BODY-FIXED TORQUES; GALILEO SPACECRAFT; SPINNING SPACECRAFT;

SPACECRAFT;

EID: 28444455275     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.12272     Document Type: Article

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