System of differential equations of aircraft spatial motion dynamics with arbitrary tensor of inertia and center of gravity position
Derivation of analytic expressions making up the basis of a mathematical model of aircraft flight dynamics for the differential equations describing the change in the rate of roll, yaw and pitch, as well as flight velocity components in projections on the body-fixed coordinate axes is presented. The...
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| Format: | Article |
| Language: | English |
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Samara National Research University
2021-07-01
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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/8926/pdf |