On-Line Trajectory Command Reshaping for Reusable Launch Vehicles
Author:
Affiliation:
1. Barron Associates Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-5439
Reference23 articles.
1. An Automated Method to Compute Orbital Re-Entry Trajectories with Heating Constraints
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