| Автор | Teo, K. L. |
| Автор | Jepps, G. |
| Автор | Moore, E. J. |
| Автор | Hayes, S. |
| Дата выпуска | 1987 |
| dc.description | 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. |
| Формат | application.pdf |
| Издатель | Cambridge University Press |
| Копирайт | Copyright © Australian Mathematical Society 1987 |
| Название | A computational method for free time optimal control problems, with application to maximizing the range of an aircraft-like projectile |
| Тип | research-article |
| DOI | 10.1017/S0334270000005476 |
| Electronic ISSN | 1446-8735 |
| Print ISSN | 0334-2700 |
| Журнал | The Journal of the Australian Mathematical Society. Series B. Applied Mathematics |
| Том | 28 |
| Первая страница | 393 |
| Последняя страница | 413 |
| Аффилиация | Teo K. L.; National University of Singapore |
| Аффилиация | Jepps G.; Weapons Systems Research Laboratory, Defence Science and Technology Organisation, Department of Defence, GPO Box 2151, Adelaide, South Australia 5001, Australia. |
| Аффилиация | Moore E. J.; University of New South Wales |
| Аффилиация | Hayes S.; University of New South Wales |
| Выпуск | 3 |
