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Reconnaissance satellite positioning and estimating method

A technology of reconnaissance satellites and Beidou satellites, which is applied in the field of satellite positioning, and can solve problems such as complex calculations, vulnerability to climate and cloud interference, coordinate transformation, etc.

Inactive Publication Date: 2013-08-14
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Claims
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AI Technical Summary

Problems solved by technology

[0004] In the traditional reconnaissance satellite positioning estimation method to detect and acquire the initial position and initial velocity of the target reconnaissance satellite at zero time, the infrared optical detector is generally used for detection and acquisition, but only the infrared radiation information of the target is received, which can be oriented but not ranged. , and is susceptible to climate influence and cloud interference, the reliability is not good enough
In addition, the traditional reconnaissance satellite positioning estimation method still has shortcomings such as the need for coordinate transformation, too many variables to be obtained, complex calculations, and insufficient estimation accuracy.

Method used

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  • Reconnaissance satellite positioning and estimating method

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Embodiment Construction

[0023] A reconnaissance satellite positioning estimation method of the present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.

[0024] Such as figure 1 As shown, in order to describe the movement of the target reconnaissance satellite, its basic coordinate system needs to be established, and the center of the earth is taken as O c As the origin, the earth's rotation axis is taken as the z-axis, pointing to the North Pole is the positive direction, and the x-axis is determined by O c Point to the 0 longitude line at zero time, and then determine the y-axis according to the right-hand system, so as to establish its basic coordinate system O c -X c Y c Z c .

[0025] The specific embodiment of the present invention provides that the initial position of the known target reconnaissance satellite at zero time is (2043922.166765m, 8186504.631471m, 4343461.714791m) and initial velocity (-5379.544693m / s, -407.09534...

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Abstract

The invention provides a reconnaissance satellite positioning and estimating method. According to the method, the initial position and the initial speed of a target reconnaissance satellite in the zero hour are acquired by using a Beidou satellite; a simplified motion equation of the target reconnaissance satellite is established, the simplified motion equation of the target reconnaissance satellite is revolved, and a nolinear differential equation model which can determine the estimated position of the target reconnaissance satellite is established; and the established nolinear differential equation model is solved, so that the estimated position of the reconnaissance satellite required to be observed at each time point is obtained, and positioning and estimating are performed. By means of the method, the reconnaissance satellite can be more accurately, more reliably and more independently positioned and estimated, a better information foundation can be provided for judging and mastering a flight intention, a flight state and a flight tendency of the target reconnaissance satellite, and the method is simple and easy to implement and high in practicability.

Description

technical field [0001] The invention relates to the technical field of satellite positioning, in particular to a reconnaissance satellite positioning estimation method. Background technique [0002] The Beidou satellite navigation system is a self-developed and independently operated global satellite navigation system that is being implemented in my country. It can provide users with all-weather, all-time high-precision and high-reliability positioning services, and has short message communication functions. The Beidou satellite navigation system consists of three parts: the space terminal, the ground terminal and the user terminal. The Beidou satellite navigation system has great strategic and economic significance for promoting the development of my country's satellite navigation and positioning business and meeting the needs of my country's military and national economy. However, the Beidou satellite navigation system can only perform real-time positioning of the objects...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01S19/42
Inventor 李洁蒋雪峰王正盛
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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