Shuttle Ascent Trajectory Optimization with Function Space Quasi-Newton Techniques
Author:
Affiliation:
1. TRW Systems Group, Redondo Beach, Calif.
2. The University of Michigan, Ann Arbor, Mich.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference17 articles.
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2. 2Ladd, H. O. "A Unified Theory for Constrained Minimization on Hilbert Space," PhD Thesis,Massachusetts Institute of Technology, Cambridge, Mass. 1968.
3. Conjugate direction methods for optimal control
4. Optimization using conjugate gradient methods
5. Computational Experience with the Davidon Method Applied to Optimal Control Problems
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