Near-optimal continuous control for spacecraft collision avoidance maneuvers via generating functions
Author:
Funder
National Research Foundation of Korea
Yonsei University
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference24 articles.
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2. A direct solution for fuel-optimal reactive collision avoidance of collaborating spacecraft;Scharf,2006
3. Energy suboptimal collision-free path reconfiguration for spacecraft formation flying;Sultan;J. Guid. Control Dyn.,2006
4. Nonlinear optimization of low-thrust trajectory for satellite formation: Legendre pseudospectral approach;Wu;J. Guid. Control Dyn.,2009
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