Abstract
The application and the performance of the neighboring optimal feedback scheme presented in Part 1 of this paper is demonstrated for the heating-constrained cross-range maximization problem of a space-shuttle-orbiter-type vehicle. This problem contains five state variables, two control variables, and a state variable inequality constraint of order zero.
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Communicated by D. G. Hull
This research was supported in part by the Deutsche Forschungsgemeinschaft under the Schwerpunktprogramm “Anwendungsbezogene Optimierung und Steuerung.”
The authors wish to express their sincere and grateful appreciation to Professor Roland Bulirsch who encouraged this work.
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Kugelmann, B., Pesch, H.J. New general guidance method in constrained optimal control, part 2: Application to space shuttle guidance. J Optim Theory Appl 67, 437–446 (1990). https://doi.org/10.1007/BF00939643
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DOI: https://doi.org/10.1007/BF00939643