Satellite-borne occultation real-time forecasting method
A space-borne and navigation star technology, applied to satellite radio beacon positioning systems, measuring devices, instruments, etc., can solve problems such as waste of hardware resources, insufficient accuracy, failure to consider visibility and real-time performance, and avoid misjudgment Or the effect of missed judgment, enhanced accuracy, and simple and easy method
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[0116] Simulation scenarios such as Figure 4 In the design shown, the satellite’s designed orbital height is 400km, the orbital inclination is designed to be 55 degrees, the attitude is designed to be oriented to the ground, and the three axes are stable. The UTC time is set from 4:00:00 on August 5, 2017 to August 6, 2017 4:00:00, the navigation constellation takes the GPS constellation as an example, the star number selection area Prn1, the spacecraft receiving antenna argument w is 40 degrees, the antenna installation pitch angle is -20, and the occultation cut angle is -30, then the antenna pitch angle gate The limit is [-22, 0]. Since the scene is designed to be three-axis stable, the antenna and the direction of motion keep coincident, so the antenna azimuth angle threshold is [-20, 20]. If the antenna has attitude maneuvers, it is necessary to introduce inertial navigation equipment. Plus the antenna orientation changes caused by attitude maneuvers. Taking time 60s as...
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