A trajectory generation framework for modeling spacecraft entry in MDAO
Author:
Funder
NASA
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference52 articles.
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3. A. Saraf, J. Leavitt, D. Chen, K. Mease, Design and evaluation of an acceleration guidance algorithm for entry, in: AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA 2003-5737, Austin, TX, 2003, http://dx.doi.org/10.2514/6.2003-5737.
4. Feasible trajectory generation for atmospheric entry guidance;Leavitt;J. Guid. Control Dyn.,2007
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