Initial deployment and near optimal control for maintaining constant distance between satellites in an elliptically orbiting constellation

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作者：
Department of Mechanical Engineering, Howard University, Washington, DC 20059, United States [1 ]
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来源：
Adv Astronaut Sci | 1600年 / 555-573期
关键词：
Compendex;
D O I：
Proceedings of the AAS/AIAA Astrodynamics Conference
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摘要：
Launching - Nonlinear control systems - Observatories - Optimal control systems - Orbits - Perturbation techniques - Satellites
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