Peculiarities of application of asymptotic methods of calculating self-oscillating aeroplane motion
DOI:
https://doi.org/10.18372/2306-1472.2.9315Abstract
Presented are the results of investigation of aeroplane motion and slipping at large angles of attack. Considered is a transformed system of differential equations describing aeroplane motion in space, in which two oscillating contours connected in rotation by special differential equations are identified. Also considered are analytical peculiarities of the process of synchronization of oscillating contours dataReferences
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Рубаник В.П. Колебания квазилинейных систем с запаздыванием. - М.: Наука, 1969. -290 с.
Кудиненко А.В. Многосвязные системы динамики полета. - К.: КВВАИУ, 1978. - 215 с.
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Кудиненко, А. В., & Котляров, В. П. (1999). Peculiarities of application of asymptotic methods of calculating self-oscillating aeroplane motion. Proceedings of National Aviation University, 2(1), 135–140. https://doi.org/10.18372/2306-1472.2.9315
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INFORMATION TECHNOLOGY