Second order optimality conditions for variable end time terminal control problems
Author:
Affiliation:
1. California Institute of Technology, Pasadena, Calif.
2. Stanford University, Stanford, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1972-932
Reference13 articles.
1. t J1 {iexT.e_*+dy'f ;'+dviP'!')(fx 6x+fu 6u-6x)dt +
2. t + ½J1[6u-6upt] TH [6u-ou0Pt] dt
Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Gain indexing schemes for low-thrust perturbation guidance;Journal of Guidance, Control, and Dynamics;1983-11
2. Low-thrust perturbation guidance;Astrodynamics Conference;1982-08-09
3. Second-Order Optimality Conditions for the Bolza Problem with Both Endpoints Variable;Journal of Aircraft;1974-04
4. Second-Order Optimality Conditions for Variable End Time Terminal Control Problems;AIAA Journal;1973-09
5. Second order optimality conditions for variable end time terminal control problems;Astrodynamics Conference;1972-08-16
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