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Information × Registration Number 0221U100702, 0119U100654 , R & D reports Title Methodology of design of precision stabilized platforms for integrated systems of aircraft special apparatus by means of perspective inertial technologies popup.stage_title Head Azarskov Valeriy M., Доктор технічних наук Registration Date 08-01-2021 Organization National Aviation University popup.description2  The object of research is a high-precision control system of the multi-axis inertial stabilized platform. The purpose of the study is to develop algorithms for the synthesis of robust control laws and to make an experimental sample of a multi-mode Coriolis vibration gyroscope for the system of inertial stabilization of moving vehicles of the general application (unmanned and manned aircraft, ground armored vehicles, surface and underwater objects). Research methods and equipment - Theory of inertial stabilization, robust control systems and Coriolis vibration gyroscopes. Methods of H2 / Hinf robust parametric optimization and Hinf robust structural synthesis. Methods of mathematical and computer modeling. The equipment of the Department of Aerospace Control Systems of NAU, as well as test equipment of the Kyiv Plant of Automation has been used for the research. Theoretical and practical results: methods of computer-aided design of robust inertially stabilized platforms based on H2 / Hinf robust parametric optimization and Hinf robust structural synthesis were developed. The block diagram of three modes of the Coriolis vibration gyroscope, the program for the signal processor, tuning, and calibration of the system were developed. Technical documentation for the manufacturing an experimental sample of the system, and methods of bench tests of the experimental sample were developed. Novelty. For the first time, a differential (third) mode of operation of the Coriolis vibratory gyroscope was developed and its self-compensating capabilities to attenuate external disturbances and internal noise were experimentally confirmed. For the first time a system of automatic switching of gyroscope modes was developed. Algorithms for calibrating system errors that have no world analogues have been developed and implemented. The degree of implementation of the results of the work is estimated at 30%. Scope: Results of the work can be used in defense technology. Product Description popup.authors Bezkorovainyi Yurii M Petrenko Oleksii V Sushchenko Olha A Tsiruk Hanna V Chikovani Valeri V popup.nrat_date 2021-03-17 Close