An ultra-high-precision attitude determination method for multi-stage composite control of spacecraft
A composite control and spacecraft technology, applied in attitude control, space navigation equipment, space navigation aircraft, etc., can solve the problem of inability to directly measure the load and the attitude information of the fast mirror, and the inability to accurately realize the multi-level attitude estimation of the spacecraft, Unable to get star-payload relative attitude and other issues
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[0075] The present invention adopts figure 1 The flow shown completes an ultra-high-precision attitude determination method for spacecraft multi-level composite control: the specific method is as follows:
[0076] (1) The multi-level composite control system of the spacecraft mainly includes the star, the active pointing ultra-static platform, the payload, and the fast mirror. The star body is used to support the active pointing ultra-stationary platform and the load; the active pointing ultra-stationary platform is installed between the load and the star platform. The payload is an optical system for high-quality imaging of the target celestial body; the fast mirror is installed inside the payload to adjust the pointing method of the payload's optical axis. The sensors in the spacecraft multi-level compound control system include: star gyroscope, load micrometer sensor, load star sensor, active pointing ultra-static platform eddy current, guide star sensor, and fast mirror e...
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