Aerostat occultation forecast method based on inertial navigation
An aerostat and navigation star technology, applied in the field of atmospheric occultation detection, can solve the problems of insufficient accuracy, failure to consider visibility and real-time performance, waste of hardware resources, etc. The effect of misjudgment or omission
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[0062] The test scene design is: the flying height of the aerostat is 20km, and the location is
[0063] (-2244788.560, 4316130.960, 4141765.440), UTC time is from 0:00:00 on September 27, 2018 to 16:00:00 on September 27, 2018, the argument angle w of the receiving antenna of the aerostat is 40 degrees, and the antenna is installed The pitch angle is -4, and the occultation cut angle is -4.5 degrees, so the antenna pitch angle threshold is [-7.5, 16]. 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 maneuvering, it is necessary to introduce inertial navigation equipment, plus the change of antenna orientation caused by attitude maneuvering. With a time step of 60s, some forecast results and reception results are shown in the table below:
[0064]
[0065] Through hardware-in-the-loop simulation, the above table is obtained, which ca...
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