Time-Optimal Rest-to-Rest Slewing of Multi-Mode Flexible Spacecraft Using ZVD Robustness Constraints
Conference, AIAA guidance navigation and control conference ; 1996 ; San Diego; CA
1996-01-01
ALL
Nos 96-3690 to 96-3929 with gaps held only; See also 6369.400F for paper nos 96-3690 to 96-3962 with gaps held on fiche
Conference paper
English
AIAA , guidance , navigation
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Slewing Multimode Flexible Spacecraft with Zero Derivative Robustness Constraints
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