AIRCRAFT ATTITUDE CONTROL
Yu. N. Zolotukhin, A. A. Nesterov
Institute of Automation and Electrometry, Siberian Branch, Russian Academy of Sciences, pr. Akademika Koptyuga 1, Novosibirsk, 630090 Russia
Keywords: летательный аппарат, угловое положение, управление ориентацией, вращающие моменты, aircraft, attitude, attitude control, torque
Abstract
The problem of control of the aircraft attitude in a three-dimensional space is considered. The attitude is described by the Euler angles between the axes of the body-fixed coordinate system and the Earth frame. A method of calculating the torque driving the aircraft to a prescribed attitude is proposed. A controller implementing this method is presented. Results of simulations are reported.
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