Coning Stability Criteria and Optimal Passive Damping of Asymmetric Spinning Spacecraft Under Thrust
Meeting; 9th, Annual space flight mechanics: Spaceflight mechanics 1999 ; 1999 ; Breckenridge; CO
01.01.1999
12 pages
Aufsatz (Konferenz)
Englisch
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Optimal Design of a Passive Coning Attenuator for Spinning Spacecraft Under Thrust
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