A computational method for free time optimal control problems, with application to maximizing the range of an aircraft-like projectile
Teo, K. L.; Jepps, G.; Moore, E. J.; Hayes, S.; Teo K. L.; National University of Singapore; Jepps G.; Weapons Systems Research Laboratory, Defence Science and Technology Organisation, Department of Defence, GPO Box 2151, Adelaide, South Australia 5001, Australia.; Moore E. J.; University of New South Wales; Hayes S.; University of New South Wales
Журнал:
The Journal of the Australian Mathematical Society. Series B. Applied Mathematics
Дата:
1987
Аннотация:
AbstractA class of non-standard optimal control problems is considered. The non-standard feature of these optimal control problems is that they are of neither fixed final time nor of fixed final state. A method of solution is devised which employs a computational algorithm based on control parametrization techniques. The method is applied to the problem of maximizing the range of an aircraft-like gliding projectile with angle of attack control.
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