Accurate Real-Time Prediction Guidance Using Numerical Integration for Reentry Spacecraft
Author:
Affiliation:
1. Japan Aerospace Exploration Agency (JAXA)
2. Mitsubishi Space Software Company, Ltd.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-4646
Reference13 articles.
Cited by 3 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. Application of an Optimal Control Allocation Scheme with Structural Load and Aero Heating Feedback for a Morphing Inflatable Aerodynamic Decelerator;2018 AIAA Atmospheric Flight Mechanics Conference;2018-01-07
2. Aerodynamic Oscillation and Attitude Control Analysis for Reentry Capsule using OREX Flight Data and Wind Tunnel Data;AIAA Guidance, Navigation, and Control Conference;2016-01-01
3. IMU-DM Integrated Navigation and Terminal Reentry Guidance for Accurate Guided Reentry Flight;AIAA Guidance, Navigation, and Control Conference;2015-01-02
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