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Information × Registration Number 0208U004998, 0107U007323 , R & D reports Title Development and testing of stabilization and attitude system of small-sized air-space vehicles/ popup.stage_title Head Grabar Ivan Grygorovych, Registration Date 29-12-2008 Organization Zhуtomуr State Technological University popup.description2 It is developed and the systems of stabilization and orientation of miniature aviakosmicheskih vehicles are explored on the basis of butt end bezkolektornogo engine of direct current. It is definite, that the system of stabilization and spatial orientation which behaves to the netno-mahovichnih systems of management mikro satellites with three fly-wheels by enginesis most perspective. This system uses adaptive kvaternionnuyu kalmanovsku yu filtration with simultaneous application of methods of kompleksovaniya, that allows to attain exactness of orientation not worse a 3 hail after the corners of tangaga and list and a 5 hail around corner prowling. Such exactness befits for majority mikro companions which do on a sun-synchronousorbit. For such system a main problem consists in creation of fly-wheel of engine with the beforehand preset parameters. The design of the modes of operations of satellite on an orbit is conducted, which showed expedience of the use in him of the magnitno-mahovichnoy system of stabilization and spatial orientation. The design of the modes of operations of magnetic-gravitation Product Description popup.authors popup.nrat_date 2020-04-02 Close