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Application of a novel optimal control algorithm to low-thrust trajectory optimizationAn application of the new optimization algorithm Static/Dynamic Control (SDC) to the design of low-thrust interplanetary trajectories is presented. The interplanetary trajectory is integrated with a multi-body force model and may include gravity assists.
Document ID
20210002619
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
hdl:2014/16157
Authors
Sims, J. A.
Whiffen, G. J.
Date Acquired
February 14, 2001
Publication Date
February 14, 2001
Publication Information
Publisher: UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review
Keywords
optimization
trajectory
low
thrust

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