Improved Sequential Convex Programming Algorithms for Entry Trajectory Optimization
Author:
Affiliation:
1. University of Tennessee, Knoxville
2. Purdue University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-0667
Reference38 articles.
1. Survey of Numerical Methods for Trajectory Optimization
2. Rapid Indirect Trajectory Optimization for Conceptual Design of Hypersonic Missions
3. Rapid, Robust Trajectory Design Using Indirect Optimization Methods
4. Indirect Trajectory Optimization for Mars Entry with Maximum Terminal Altitude
5. Numerical Techniques for the Optimal Control Problem
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