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Method for tracking lunar probe by using earth station

A technology for detectors and earth stations, which is applied in the field of tracking lunar detectors by earth stations, which can solve problems such as earth station deviation, lack of tracking, and inappropriate selection of interpolation points, so as to improve efficiency and accuracy, and ensure accuracy performance, reducing complexity

Active Publication Date: 2011-02-09
NAT ASTRONOMICAL OBSERVATORIES CHINESE ACAD OF SCI
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Problems solved by technology

However, when using the Lagrangian polynomial interpolation method, it may be due to the inappropriate selection of interpolation points that the phenomenon of being interpolated cannot be better approximated with the increase of the interpolation polynomial degree (that is, the Runge phenomenon), thereby affecting Accuracy of Lunar Probe's Precise Ephemeris
[0006] The above-mentioned defects will directly lead to errors in the process of tracking the lunar probe by the earth station or even errors that cannot be tracked, which will affect the successful implementation of the lunar exploration project.

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Embodiment Construction

[0036] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be described in further detail below in conjunction with specific embodiments and with reference to the accompanying drawings.

[0037] Such as figure 1 As shown, the present invention proposes a method for tracking the lunar probe by using the earth station for tracking the lunar probe. Calculate the synthetic perturbation ephemeris, and output the calculation results to the synthetic perturbation ephemeris file; calculate the earth shadow forecast, moon shadow forecast and ascending node forecast; calculate the lunar probe relative to the earth and the substar point of the moon Forecasting; calculating the forecast of the sun relative to the earth and the sub-star point of the moon; calculating the position of the lunar probe relative to the earth station; calculating lunar occlusion; generating the observation and forecast file of the earth stat...

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Abstract

The invention discloses a method for tracking a lunar probe by using an earth station. The method comprises the following steps of: performing orbit determination on the lunar probe to generate a precise orbital element for the lunar probe to run on a lunar orbit; calculating a synthetic perturbation ephemeris according to the precise orbital element for the lunar probe to run on the lunar orbit and outputting a calculation result to a synthetic perturbation ephemeris file; calculating earth shadow forecast, moon shadow forecast and ascending node forecast, calculating substellar point forecast of the lunar probe relative to earth and moon and calculating the substellar point forecast of the sun relative to earth and moon; calculating the position of the lunar probe relative to the earth station; calculating shelter of the moon and forecasting the condition that the lunar probe is sheltered by the moon; generating an earth station observation forecast file; and tracking the lunar probe by the earth station according to the observation forecast file. By the method, the measurement and control of the lunar probe and the receiving of probe data are tracked by using the earth station.

Description

technical field [0001] The invention relates to the technical field of tracking a deep-space probe by using an earth station, in particular to a method for tracking a lunar probe by using an earth station. Background technique [0002] Deep space exploration is the first step for human beings to understand the earth, the solar system and the universe, and then investigate, explore and settle other celestial bodies in the solar system. Deep space exploration mainly includes lunar exploration, planetary exploration, interplanetary exploration and interstellar exploration. Through deep space exploration, it can help humans study the origin, evolution and current status of the solar system and the universe, further understand the formation and evolution of the earth's environment, and understand the relationship between space phenomena and the earth's natural systems. From a practical and long-term point of view, the exploration and development of deep space has very important ...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01S13/72G01S7/02G01S13/66
Inventor 温卫斌付强嫣俊洁王涛沈勇王芳张洪波苏彦任鑫刘建军李春来
Owner NAT ASTRONOMICAL OBSERVATORIES CHINESE ACAD OF SCI
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