A Direct Method for Approach and Landing Trajectory Reshaping with Failure Effect Estimation
Author:
Affiliation:
1. Naval Postgraduate School
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-4772
Reference17 articles.
1. Dynamic Inversion-Based Adaptive/Reconfigurable Control of the X-33 on Ascent
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4. On-Line Trajectory Command Reshaping for Reusable Launch Vehicles
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