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Information × Registration Number 0221U104082, (0119U103350) , R & D reports Title The development of direct Lyapunov method based on nonlinear integral inequalities and its application to the problems of motion stability of aerospace systems popup.stage_title Розробка алгоритмів, які дозволяють виключити переключення в системі управління боковим рухом квадрокоптера при відмові відповідного датчика Head Martyniuk Anatolii A., Registration Date 02-03-2021 Organization S.P.Timoshenko Institute of Mechanics popup.description1 The development of constructive generalization of direct Lyapunov method to be applied for the perturbed motion investigation of aerospace systems described by nonlinear equations with ordinary and fraction-like derivatives of the system state vector popup.description2 The problem of increasing the reliability of the quadcopter control system by introducing a dynamic observer into the system is considered. In this regard, the inverse problem of the synthesis of the optimal regulator is considered. An algorithm for the synthesis of a quadcopter side motion regulator is proposed, which guarantees the stability of the system in the event of a failure of the roll sensor measuring the angle.  Product Description popup.authors Ivanov Igor L. Larin Volodymyr B. Lukianova Tetiana O. Martyniuk Anatolii A. Martyniuk-Cherniienko Yuliia A. Nikitina Neli V. Rasshyvalova Svitlana M. Talimonova Olha Yu. Khoroshun Anatolii S. Chernetska Larysa M. popup.nrat_date 2021-03-02 Close

Information × Registration Number 0221U104082, (0119U103350) , R & D reports Title The development of direct Lyapunov method based on nonlinear integral inequalities and its application to the problems of motion stability of aerospace systems popup.stage_title Розробка алгоритмів, які дозволяють виключити переключення в системі управління боковим рухом квадрокоптера при відмові відповідного датчика Head Martyniuk Anatolii A., Registration Date 02-03-2021 Organization S.P.Timoshenko Institute of Mechanics popup.description1 The development of constructive generalization of direct Lyapunov method to be applied for the perturbed motion investigation of aerospace systems described by nonlinear equations with ordinary and fraction-like derivatives of the system state vector popup.description2 The problem of increasing the reliability of the quadcopter control system by introducing a dynamic observer into the system is considered. In this regard, the inverse problem of the synthesis of the optimal regulator is considered. An algorithm for the synthesis of a quadcopter side motion regulator is proposed, which guarantees the stability of the system in the event of a failure of the roll sensor measuring the angle.  Product Description popup.authors Ivanov Igor L. Larin Volodymyr B. Lukianova Tetiana O. Martyniuk Anatolii A. Martyniuk-Cherniienko Yuliia A. Nikitina Neli V. Rasshyvalova Svitlana M. Talimonova Olha Yu. Khoroshun Anatolii S. Chernetska Larysa M. popup.nrat_date 2021-03-02 Close