Space-based bearing-only measurement differential evolution one-time precise orbit determination method

A differential evolution, angle measurement technology, applied in the field of satellite orbit determination, can solve the problems of calculation error, divergence, deviation of calculation results from the true value, etc., and achieve the effect of improving the accuracy of orbit determination

Active Publication Date: 2020-02-11
BEIHANG UNIV
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Problems solved by technology

Existing orbit optimization methods all have high requirements for initial value selection, and initial values ​​that deviate far from the real orbit data will cause inaccurate or even divergent orbit determination results.
In addition, the existing orbit optimization methods all perform linear approximation on the orbit transfer matrix during the

Method used

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  • Space-based bearing-only measurement differential evolution one-time precise orbit determination method
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  • Space-based bearing-only measurement differential evolution one-time precise orbit determination method

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Embodiment 1

[0156] Simulation Verification - Orbit Determination Experiment

[0157] The present invention selects FengYun1C space debris as the observation target, and its orbit data is taken from the public TLE data set [celestrak.com]. The orbital height of FengYun1C is close to that of a sun-synchronous satellite. The orbit of the observation platform is selected with reference to Fengyun-1. The semi-major axis of the observation platform is a=7237km, the eccentricity is e=0, and the orbital inclination is 98.88 degrees. The experiment randomly selects space debris with different spatial distributions as observation targets.

[0158] In the experiment, the influence of J2 perturbation was considered for the orbit data, and STK was used to generate satellite orbit position, velocity data and angle data, and the method was verified in matlab. The angle data observation accuracy is 5", the sampling frequency is 1HZ, and the effective observation distance is 5000km. The experiment select...

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Abstract

The invention aims at a problem of outer space noncooperative target precise orbit determination, and provides a space-based bearing-only measurement differential evolution one-time precise orbit determination method. In the method, based on thinking of least square batch processing orbit determination, a differential evolution algorithm is used to directly optimize an orbit determination objective function, thus, a situation of misconvergence or convergence errors, which may happen in a solving process of the direct least square batch processing method, can be avoided, moreover, a secondary orbit determination process required by general precise orbit determination is not needed, and an aim of one-time precise orbit determination can be realized. The method provided by the invention constructs a target orbit parameter vector based on an orbital kinetic equation description form, and under the situation of only using angle observation data, accurately solves an orbit spatial position and speed of the target at particular moment. A simulation experiment shows that an angle measurement sequence with precision of 5 seconds of arc is used, effective observation distance is in a range of 5000 kilometers, orbit determination precision of the method is as high as hundreds of meters order of magnitude, and the method can be used for a satellite orbit determination task.

Description

technical field [0001] The invention belongs to the technical field of satellite orbit determination, and in particular relates to a space-based differential evolution method for one-time precise orbit determination with only angle measurement. Background technique [0002] There are a large number of non-cooperative targets such as space debris and malfunctioning spacecraft in space. These targets have caused great safety hazards to the flight of spacecraft in space. Therefore, surveillance of non-cooperative targets is of great significance in space missions. Space surveillance can be divided into ground-based surveillance and space-based surveillance. Compared with ground-based surveillance (GBSS), space-based surveillance is not restricted by the location and number of observation stations, and more observation data can be obtained according to mission requirements. In space-based surveillance, optical imaging is the main observation method for non-cooperative targets....

Claims

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Application Information

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IPC IPC(8): G01C21/24
CPCG01C21/24
Inventor 郑红东楷涵黄镐孙玉泉
Owner BEIHANG UNIV
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