Инд. авторы:	Zolotukhin Y.N., Nesterov A.A.
Заглавие:	Aircraft Attitude Control
Библ. ссылка:	Zolotukhin Y.N., Nesterov A.A. Aircraft Attitude Control // Optoelectronics, Instrumentation and Data Processing. - 2015. - Vol.51. - Iss. 5. - P.456-461. - ISSN 8756-6990. - EISSN 1934-7944.
Внешние системы:	DOI: 10.3103/S8756699015050040; SCOPUS: 2-s2.0-84949224400; WoS: 000421011800004;
Реферат:	eng: 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.
Ключевые слова:	torque; attitude control; attitude; aircraft;
Издано:	2015
Физ. характеристика:	с.456-461