Near-optimum guidance schemes for abort landing flight in a windshear

[摘要] 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.

[发布机构] Rice University

[效力级别] engineering