Improved Secant Method Applied to Boost Trajectory Optimization
Author:
Affiliation:
1. Lewis Industries, Kansas City, Mo.
2. University of Texas at Austin, Austin, Texas
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.57166
Reference17 articles.
1. A Steepest-Ascent Method for Solving Optimum Programming Problems
2. Denham, W.F. ' 'Steepest Ascent Solution of Optimal Programming Problems," Ph.D. Dissertation,Harvard University, 1973.
3. Rapid convergence to optimum solutions using a Min-H strategy.
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