Autonomous navigation semi-physical simulation test system based on biconical infrared and star sensors
A star sensor and test system technology, applied to instruments, measuring devices, etc., to achieve the effect of easy implementation and simple and convenient control method
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[0025] Such as figure 1 As shown, the present invention mainly includes a double-cone infrared earth sensor, a double-chord wide earth simulator, a star sensor, a dynamic star simulator, a single-axis turntable, an attitude orbit simulator, a navigation computer, and a control computer. The dual-cone infrared is installed on a single-axis turntable. The single-axis turntable can drive the dual-cone infrared to rotate to simulate the rolling attitude of the satellite. The double-cone infrared earth sensor observes the double-chord wide earth simulator, and the star sensor observes the dynamic star simulator. The attitude orbit simulator uses the satellite orbit dynamics model to calculate the satellite attitude orbit, and the calculation results are sent to the control computer and the navigation computer as reference data. The control computer generates a chord width command based on the reference attitude orbit data to control the chord width change of the earth simulator to s...
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