Adaptive Terminal Guidance for Hypervelocity Impact in Specified Direction
By Ping Lu, David B. Doman, J. Schierman. 2005
212 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/9ca10b96ebde801fa99985917707d39f2de9244d
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In Aerospace Engineering
In Computational Mechanics
Citations in the corpus
- Impact Time and Angle Guidance With Sliding Mode Control (2009, methodology): “develop adaptive control laws for obtaining specified impact angles, and apply their approach to the reentry guidance of a hypersonic gliding vehicle [7].”