method of determination of u043du0435u043fu0435u0440u043fu0435u043du0434u0438u043au0443u043bu044fu0440u043du043eu0441u0442u0438 axes sensor angle dynamically customize the gyroscope with u043fu0435u0440u043fu0435u043du0434u0438u043au0443u043bu044fu0440u043du043eu0441u0442u0438 axes sensor point

摘要

method u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 u043du0435u043fu0435u0440u043fu0435u043du0434u0438u043au0443u043bu00a0u0440u043du043eu0441u0442u0438 axes sensor angle dynamically customize the gyroscope with u043fu0435u0440u043fu0435u043du0434u0438u043au0443u043bu00a0u0440u043du043eu0441u0442u0438 axes sensor point u0432u043au043bu044eu0447u0430u044eu0449u0438 in the introduction u043fu043eu0441u0442u043eu00a0u043du043du043eu0433u043e u0441u043cu0435u0449u0435u043du0438u00a0 in each of the channels of the correction and measurement of changes in the sensors of the u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 so that, with a view to improving the u0448u0435u043du0438u00a0 accuracy.measurement of changes in the sensors of the u043fu0440u043eu0438u0437u0432u043eu0434u00a0u0442 in two u043du0430u043fu0440u0430u0432u043bu0435u043du0438u00a0u0445 u0432u0440u0430u0449u0435u043du0438u00a0 rotor gyroscope and u043du0435u043fu0435u0440u043fu0435u043du0434u0438u043au0443u043bu00a0u0440u043du043eu0441u0442u044c axes sensor on the u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 formulas;= x + y;;where x, y and the angle between the sensor and the angle sensor u043eu0441u00a0u043cu0438 installed on one axis;;ix, Iy change of current in the channel u043cu043eu043cu0435u043du0442u043du043eu043c sensor correction, with one bar corresponds to the u043fu0440u00a0u043cu043eu043cu0443 direction u0432u0440u0430u0449u0435u043du0438u00a0 rotor, and two strokes on the u0440u0430u0442u043du043eu043cu0443;;Kx, ky - steep current sensors on respective channels for correction.