Optimal slew-rate-limited guidance for combined formation establishment and reconfiguration of inspector satellite with exclusion cone
Document Type
Conference Proceeding
Publication Date
2-7-2017
Source Publication
27th AAS/AIAA Space Flight Mechanics Meeting, 2017
Recommended Citation
Prince, E., Cobb, R. G., & Hess, J. A. (2017). Optimal slew-rate-limited guidance for combined formation establishment and reconfiguration of inspector satellite with exclusion cone. 27th AAS/AIAA Space Flight Mechanics Meeting, 2017, 160, 823–841.
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