Application of a Near-Optimal Feedback Guidance Algorithm to Spacecraft in Dynamically Complex Environments
A near-optimal feedback guidance algorithm is applied to several different applications in the Circular-Restricted Three Body Problem and in proximity operations in LEO modeled by Keplerian motion. In both scenarios gravitational perturbations are introduced in order to assess the algorithm's r...
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| Language: | en_US |
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The University of Arizona.
2017
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| Online Access: | http://hdl.handle.net/10150/622903 http://arizona.openrepository.com/arizona/handle/10150/622903 |