Comparison of Implicit Integration Methods for Solving Aerospace Trajectory Optimization Problems
Author:
Affiliation:
1. NASA Glenn Research Center
2. Boeing Phantom Works
3. NASA Kennedy Space Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-6033
Reference33 articles.
1. Direct and indirect methods for trajectory optimization
2. Paris, S.W., Hargraves, C.R., et. al. "Optimal Trajectories by Implicit Simulation (Version 1.2)", WRDC-TR-88-3057 Vols. I-IV,November 1988
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