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

Active Publication Date: 2019-02-19
天津讯联科技有限公司 +1
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AI Technical Summary

Problems solved by technology

[0004] The existing occultation prediction algorithm is mainly calculated by using simulation software, and then placed in the device in advance, without considering the visibility and real-time performance in practical applications, so the accuracy rate is insufficient, resulting in a waste of hardware resources

Method used

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  • Satellite-borne occultation real-time forecasting method
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  • Satellite-borne occultation real-time forecasting method

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Embodiment

[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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Abstract

The invention discloses a satellite-borne occultation real-time forecasting method. The method comprises the steps of: obtaining the position velocity of a spacecraft according to the positioning device of an occultation detector; calculating the orbit parameter of the spacecraft; calculating the position velocity of the spacecraft and all navigation stars after 10s; calculating the pitch angle, the azimuth angle, the tangent point height of all navigation stars and the antenna azimuth angle of the spacecraft; judging whether the obtained pitch angle Elv, the tangent point height Hight and theantenna azimuth angle satisfy the threshold of the occultation event extrapolating the time for 30 s and 1 min, repeating the above calculation and determination processes if satisfied; and determining that the navigation star is the occultation if all are satisfied. The method of the invention adopts a continuous arc to judge the occultation event through an inertial navigation device, and enhances the accuracy of the forecasting result. The method is simple and easy to implement, and has important application value for real-time forecasting.

Description

technical field [0001] The present invention relates to the technical field of atmospheric occultation detection, in particular to a spaceborne real-time occultation prediction method, which utilizes spaceborne atmospheric occultation detection equipment and initialized hardware equipment to predict the occurrence of occultation events in advance and provide initial information for quickly capturing occultation events. condition method. Background technique [0002] The success of the GPS / MET experiment has verified the great value of GNSS radio occultation technology for the detection of the earth's atmosphere. With the development of GNSS radio occultation technology, more and more countries pay attention to occultation technology. The occultation event refers to the physical change phenomenon that the navigation signal of the GNSS satellite passes through the ionosphere and atmosphere on the earth's surface and produces bending. Occultation technology refers to the tech...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01S19/42G01S19/47G01S19/08
CPCG01S19/08G01S19/42G01S19/47
Inventor 温凯刘永成张春泽李昌兴杨荣康郭启云
Owner 天津讯联科技有限公司
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