OPTIMAL AIRCRAFT CONTROL SYNTHESIS BASED ON THE EQUATIONS OF NON-LINEAR DYNAMICS
The article considers the technique of the synthesis of non-linear aircraft control systems by flight optimization us- ing inverse dynamics problems. To synthesize control algorithms a non-linear model of aircraft flight and trajectory movement is used. The authors define method stages of flying lev...
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| Автори: | , |
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| Формат: | Artigo |
| Мова: | Russo |
| Опубліковано: |
Moscow State Technical University of Civil Aviation
2017-06-01
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| Серія: | Научный вестник МГТУ ГА |
| Предмети: | |
| Онлайн доступ: | https://avia.mstuca.ru/jour/article/view/1089 |
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