Aerodynamic Oscillation and Attitude Control Analysis for Reentry Capsule using OREX Flight Data and Wind Tunnel Data
Author:
Affiliation:
1. Japan Aerospace Exploration Agency (JAXA)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-1131
Reference9 articles.
1. Accurate Real-Time Prediction Guidance Using Numerical Integration for Reentry Spacecraft
2. Overview of Orion Crew Module and Launch Abort Vehicle Dynamic Stability (Invited)
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