Method for constructing testing environment of satellite control system

A technology of satellite control system and construction method, which is applied in the direction of electrical testing/monitoring, etc., can solve the problems that the test environment cannot meet the satellite test requirements, difficulty in building and transplanting, and different test environments, so as to improve the establishment efficiency and speed up the development progress , the effect of saving manpower

Inactive Publication Date: 2013-09-04
BEIJING INST OF CONTROL ENG
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Problems solved by technology

Therefore, the test environments of different systems are different, they cannot be used universally, it is difficult to build and transplant, and the requirements for people are high.
[0006] With the increase of satellite development tasks, the establishment and use mode of the original test environment can no longer meet the rapidly growing demand for satellite testing

Method used

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  • Method for constructing testing environment of satellite control system
  • Method for constructing testing environment of satellite control system

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Embodiment Construction

[0020] The principle of the ground simulation test environment for the satellite control system is as follows: figure 1 shown.

[0021] The ground dynamics model is run by the ground test equipment, and according to the mathematical model of each sensor, the sensor signals required for the closed-loop of the on-board equipment are generated, the real signal is generated by the signal source of the ground test equipment, and the sensor signal is collected by the on-board controller. The output of the actuator is controlled by calculation, and then the output of the actuator on the star is collected by the hardware of the ground test equipment, and then output to the ground dynamics model through the actuator component model, thus forming a complete closed circuit.

[0022] The establishment of the ground test environment is to establish a closed loop between the satellite and the ground. It is a challenge to quickly build a test environment, facilitate transplantation, and reco...

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Abstract

The invention discloses a method for constructing a testing environment of a satellite control system. The method comprises the following steps of classifying component parts of a satellite control system to be tested, establishing a standardized model of each part and performing modular packaging; classifying input and output ports in each standardized model according to respective signal type, and counting various signals of a single part model; performing number maximized configuration on hardware interfaces of test equipment according to types and numbers of parts possibly used by different satellite control systems; and fixedly connecting hardware interface signals of the test equipment and modular models, and fixedly connecting part models and a dynamical model to form a closed loop. By the method, the current situation of constructing the testing environment of the satellite control system by 'customizing for each satellite' is changed, the development speed is improved, the efficiency of constructing the testing environment is improved by modularizing and standardizing the interfaces, the method is convenient to use, and manpower, material resources and time cost are saved.

Description

technical field [0001] The invention belongs to aerospace testing technology and relates to rapid establishment, recovery and transplantation of a testing environment during ground testing. Background technique [0002] The satellite control system is an important service subsystem of the satellite. It is responsible for the attitude and orbit control of the satellite. How to verify the correctness of the control scheme more effectively on the ground is the key to the problem. [0003] The ground test verification work includes mathematical simulation and physical simulation. The difference between physical simulation and mathematical simulation is that in physical simulation, the real components of the satellite need to be connected, and some simulators are used to simulate various states of the satellite in orbit. This kind of simulation test is called "mock flight test". Because it is a real component, the physical characteristics of the component are closer to the real ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B23/02
Inventor 王胜刚周剑敏曹永梅王哲袁军潘立鑫
Owner BEIJING INST OF CONTROL ENG
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