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An Analytical Calculation Method Applicable to Geostationary Satellite Fixed-point Control Planning

A fixed-point control and calculation method technology, which is applied in the field of analytical calculation, can solve the problems of cumbersome analytical calculation method process and excessive calculation amount, and achieve the effect of simple process, simple iterative process and small calculation amount

Active Publication Date: 2022-08-05
CHINA XIAN SATELLITE CONTROL CENT
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Problems solved by technology

[0003] The purpose of the present invention is to provide an analytical calculation method suitable for fixed-point control planning of geostationary satellites, so as to solve the technical problems of the existing analytical calculation method for fixed-point control planning of geostationary satellites.

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  • An Analytical Calculation Method Applicable to Geostationary Satellite Fixed-point Control Planning
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  • An Analytical Calculation Method Applicable to Geostationary Satellite Fixed-point Control Planning

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Embodiment Construction

[0040] The present invention will be described in detail below with reference to the accompanying drawings and specific embodiments.

[0041] An analytical calculation method suitable for the fixed-point control planning of the geosynchronous satellite of the present invention is realized as follows: firstly, according to the fixed-point capture orbit control model, the fixed-point capture control terminal constraint model is established, and the three-pulse control timing constraint model and the pulse size constraint model are determined, Then, according to the time interval of the control pulses, the size of the three-pulse and its control timing are solved in three cases, and finally the three-pulse control parameters satisfying the terminal condition under the full perturbation condition are determined by perturbation iteration, such as Figure 1 to Figure 2 shown, follow the steps below:

[0042] Step 1. Establish a fixed-point capture orbit control model, determine the ...

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Abstract

The present invention is an analytical calculation method suitable for a geosynchronous satellite fixed-point control plan, which is specifically implemented according to the following steps: step 1, establishing a fixed-point capture orbit control model, and determining control target variables and design variables; step 2, establishing a fixed-point capture orbit control model according to the Fixed-point capture control terminal constraint model; Step 3, determine the three-pulse constraint model according to the fixed-point capture orbit control model and the fixed-point capture control terminal constraint model, and calculate the size of the three-pulse and its control timing; Step 4, use the perturbation iteration method to determine Three-pulse control parameters that satisfy terminal conditions under full perturbation conditions. The invention establishes a three-pulse constraint model through the fixed-point capture orbit control model and the fixed-point capture control terminal constraint model, and can cover all possible working conditions of the fixed-point capture control through three situations, and the iterative process is simple, and it can converge to 2-3 times. The target value, the process is simple, and the amount of calculation is small.

Description

technical field [0001] The invention belongs to the technical field of satellite navigation information processing, and relates to an analytical calculation method suitable for geosynchronous satellite fixed-point control planning. Background technique [0002] Before entering the working orbit, the geostationary orbit satellite needs to perform fixed-point acquisition control, which requires the orbital height, orbital eccentricity size and direction, and fixed-point position to meet the requirements, which is essentially a three-pulse orbital transfer problem in the plane. How many times the fixed-point capture control is carried out, at what time, whether the control times and control timing can be adjusted, and understanding and grasping the distribution of the follow-up control can enable the task personnel to make reasonable arrangements for the follow-up work. The basic idea of ​​fixed-point acquisition control is: within the existing longitude deviation, at an approp...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/24G06F17/11
CPCB64G1/242G06F17/11
Inventor 沈红新曹静蒯政中李恒年
Owner CHINA XIAN SATELLITE CONTROL CENT
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