Optimal command control of hypersonic aircraft flight path in conditions of atmospheric disturbances
Disturbed flight of a hypersonic vehicle in accelerated climb is analyzed. Disturbances are deviations of atmospheric density from the values of a standard model. The following concepts and definitions are used in the paper. The nominal optimal angle-of-attack control program is the angle-of-attack...
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| Format: | Article |
| Language: | English |
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Samara National Research University
2020-05-01
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| Series: | Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение |
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| Online Access: | https://journals.ssau.ru/vestnik/article/viewFile/7769/7646 |