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White Paper: A Numerical Study Of Orbit Lifetime
We examine how the issues of uncertain atmospheric behavior, selection of an a prior atmospheric density model affect orbital predictions
Read MoreWhite Paper: Approximate Optimal Feedback Guidance For Soft Lunar Landing Using Gaussian Process Regression
In this paper, the lunar landing guidance problem is solved by adopting a particular implementation of dynamic programming, namely optimal feedback.
Read MoreWhite Paper: Preparation of Papers for AIAA Technical Conferences
This work uses simple orbital dynamics to initially assess the vulnerability of a satellite to a missile.
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