method for spatial reorientation and changes the parameters of movement of spacecraft

摘要

the invention relates to control systems spatial position of spacecraft (sc) through the artificial establishment of transitional chaotic re u0436u0438u043cu0430 and involving a chaotic motion for passive achieve dynamic parameters.method based on the artificial initiation homo / u0433u0435u0442u0435u0440u043eu043au043bu0438u043du0438u0447u0435u0441u043au043eu0433u043e chaos through the creation of a special type of rotational moment in u044du043bu0435u043au0442u0440u043eu0434u0432u0438u0433u0430u0442u0435u043bu0435 set the government consistently including the following dynamic phases: primary regular movement / chaotic movement / final regular movement with the new di u043du0430u043cu0438u0447u0435u0441u043au0438u043cu0438 parameters.the proposed method developed device constitutes a flywheel rotor is provided to set the law in rotational movement motor, boot in the creation, on one of the main axes and u043eu0442u0440u0430u0431u0430u0442u044bu0432u0430u044eu0449u0438u043c special law administration its rotational moment.the technical result is a passive orientation in space through the use of the natural properties of loudly outraged homo / u0433u0435u0442u0435u0440u043eu043au043bu0438u043du0438u0447u0435u0441u043au043eu0439 dean u0430u043cu0438u043au0438 (homo / u0433u0435u0442u0435u0440u043eu043au043bu0438u043du0438u0447u0435u0441u043au043eu0433u043e chaos), as well as the change in the quality of the dynamic regime of the movement and its quantitative characteristics, including u043fu0430u0440u0438u0440u043eu0432u0430u043du0438u0435 off normal spatial orientation and uncontrolled rotation.