NASA NTRS · 20210002619
Application of a novel optimal control algorithm to low-thrust trajectory optimization
Abstract
An 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.
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Sims, J. A., Whiffen, G. J.. 2001-02-14. Application of a novel optimal control algorithm to low-thrust trajectory optimization. https://ntrs.nasa.gov/citations/20210002619
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