OPTIMUM DEBOOST ALTITUDE FOR SPECIFIED ATMOSPHERIC ENTRY ANGLE
Author:
Affiliation:
1. The Marquardt Corporation, Van Nuys, Calif.
2. Lockheed Aircraft Corporation, Burbank, Calif.
3. University of Southern California, Los Angeles, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.1880
Reference4 articles.
1. Controlled Recovery of Nonliving Satellites
Cited by 10 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Multi-Process Integrated Planning and Guidance for Return of Reusable Aircraft Under Time Constraint;IEEE Access;2020
2. Atmospheric Interface Reentry Point Targeting Using Aerodynamic Drag Control;Journal of Guidance, Control, and Dynamics;2015-03
3. Optimal Deorbit Guidance;Journal of Guidance, Control, and Dynamics;2012-01
4. Some design aspects of space shuttle orbiters;Progress in Aerospace Sciences;1972-01
5. OPTIMAL CONTROL FOR SYNERGETIC PLANE CHANGE;Proceedings of the XXth International Astronautical Congress;1972
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