A LOWER BOUND COMPUTATION METHOD USING ENERGY-STATE APPROXIMATION AND ITS APPLICATION TO SUPERSONIC AIRCRAFT SHORTEST PATH PROBLEMS
Author:
Affiliation:
1. The University of Tokyo
Publisher
The Operations Research Society of Japan
Subject
Management Science and Operations Research,General Decision Sciences
Link
https://www.jstage.jst.go.jp/article/jorsj/41/2/41_KJ00001201851/_pdf
Reference12 articles.
1. 1) ARDEMA M. D. Solution of The Minimum Time-to-Climb Problem by Matched Asymptotic Expansions. AIAA Journal. (1976) vol.14, p.843-850.
2. 2) ATHANS M. Optimal Control. Mcgraw-Hill. (1966)
3. 3) BELLMAN R. E. Dynamic Programming. Princeton University Press. (1957)
4. 4) BRYSON A. E. Jr. Energy-State Approximation in Performance Optimization of Supersonic Aircraft. Journal of Aircraft. (1969) vol.6, p.481-488.
5. 5) BRYSON A. E. A Steepest-Ascent Method for Solving Optimum Programming Problems. Journal of Applied Mechanics. (1962) vol.29, p.247-257.
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