Determination of optimal trajectory under design constraints for a satellite launch vehicle
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference10 articles.
1. A steepest ascent method for solving optimum programming problems;Bryson;J. Appl. Mech.,1962
2. Optimal programming problems with inequality constraint—I: Necessary conditions for extremal solutions;Bryson;AIAA J.,1963
3. Optimal programming problems with inequality constraints—II: Solution by steepest ascent;Denham;AIAA J.,1964
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