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Information × Registration Number 0222U001317, 0121U111522 , R & D reports Title Implementation of the long-term development plan of the scientific direction "Technical Sciences" of the National Technical University of Ukraine "Igor Sikorsky Kyiv Polytechnic Institute" popup.stage_title Head Ilchenko Mykhailo Yu., Registration Date 26-01-2022 Organization National Technical University of Ukraine "Igor Sikorsky Kyiv Polytechnic Institute" popup.description2  The object of research is the processes of creating CubeSat satellites for remote sensing of the Earth. The purpose of the work is to develop design documentation for Cubesat nanosatellites of remote sensing of the Earth with a resolution of 30 meters - PolyITAN-30 and 2 (4) m - PolyITAN-12U conducting appropriate ground tests and trials. Based on the results of research: the concept of building nanosatellites in CubeSat format; developed and ensured reliable operation of receiving and transmitting equipment; outlined options and principles of construction, placement of onboard equipment to perform the main function - remote sensing of the Earth; the concept of building a power supply system from high-efficiency solar panels with a total area of ​​0.31 m2, which provide an integrated daily power of 38.5 W; the chosen concept of construction of all onboard equipment and its interaction at the program level; the concept of construction of the onboard equipment of orientation and stabilization at all stages of a life cycle is chosen, methods of calibration and adjustment of sensors of the primary information of system of orientation of micro- and nano-satellites are developed; Algorithms for controlling the flywheel engine and selecting its parameters have been developed, which allow calming the nanosatellite at the initial stage of launching into orbit without unloading the flywheel engines, which reduces time and energy consumption and increases the reliability of the initial stage of flight; an algorithm for determining the parameters of physical fields: the vector of the Earth's magnetic field and the vector of solar radiation at each point of the satellite's orbit to ensure the operation of algorithms for determining the orientation of the micro or nanosatellite; control algorithms for Cubesat satellites at the stages of calming and stabilization of the angular position are synthesized; Product Description popup.authors Yefimenko Yana V Adamenko Volodymyr O Antypenko Ruslan V. Barannyk Oleksandr A. Bezuhlyi Oleh A Byk Mikhajlo V Burnashev Vitalii Vitaliiovych Vasylkevych Oleksandr I Volovyk Dmytro V Dudka Oleksandr Ivanovych Dusheyko Mikhail Grigorovich Zinher Yana L Zakharchenko Oksana S. Zbrutskyi Oleksandr V. Zyev Igor O. Kaminskyj Sеrgiy V. Karpets Myroslav Vasylovych Kovalenko Yevgen Y. Korobko Ivan Vasylovych Kotlyar Sergei Anatolievich Kratko Oleksii O Linyucheva Olga V Martynyuk Sergiy Yevstafiyovich Myronov Dmytro V. Myronchuk Oleksandr Yu. Novosad Andrii A Pinchuk Artem I. Pavlyk Petro M Pershyn Mykola O Ponomarenko Serhii O Popsui Volodymyr I Poshtarenko Yurii H Pukha Hennadii S Pukha Serhii P. Rassamakin Boris M. Rudakov Eduard V. Sydorenko Yurii M. Stefurak Mykola V STETSIUK LIUDMYLA V Sushko Iryna O Trunov Viktor Yu Khominich Viktor I Khristenko Vadim V Tsybenko Olexandr Sergeevich Shpylka Oleksandr O. Yavorskyi Yurii Vasylovych popup.nrat_date 2022-03-09 Close