Near-optimum guidance schemes for abort landing flight in a windshear
Date
1988
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Abstract
In this thesis, near-optimum guidance schemes for abort landing trajectories in a windshear are investigated. These near-optimum guidance schemes are based on the properties of the optimum trajectories. The survival capability in a severe windshear is studied. The optimal trajectories are used as ideal benchmarks against which the goodness of any guidance scheme can be measured.
Description
Advisor
Degree
Master of Science
Type
Thesis
Keywords
Aerospace engineering, Mechanical engineering
Citation
Wang, Jyhshing Jack. "Near-optimum guidance schemes for abort landing flight in a windshear." (1988) Master’s Thesis, Rice University. https://hdl.handle.net/1911/13326.
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