Satellite flight control closed loop simulation system based on component simulator

A flight control and closed-loop simulation technology, applied in the field of satellite simulation testing, can solve the problems of increasing the cost and complexity of the simulation system, affecting the credibility of the simulation results, etc., shortening the development cycle, shortening the development cycle, and improving the credibility of the simulation Effect

A flight control and closed-loop simulation technology, applied in the field of satellite simulation testing, can solve the problems of increasing the cost and complexity of the simulation system, affecting the credibility of the simulation results, etc., shortening the development cycle, shortening the development cycle, and improving the credibility of the simulation Effect

CN102411313AInactive Publication Date: 2012-04-11TSINGHUA UNIV

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  • Satellite flight control closed loop simulation system based on component simulator
  • Satellite flight control closed loop simulation system based on component simulator
  • Satellite flight control closed loop simulation system based on component simulator

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Experimental program
Comparison scheme
Effect test

Embodiment 1

[0034]An embodiment of the present invention provides a satellite flight control closed-loop simulation system based on a component simulator, which is applied to a system including a dynamic simulation server, a sensor simulator, an actuator simulator and an on-board computer, such as figure 1 As shown in FIG. 1 , it is a flow diagram of a closed-loop simulation of a simulation system provided by an embodiment of the present invention, including the following steps:

[0035] Step 101: The dynamics simulation server calculates the orbit parameter information and attitude quaternion information of the current satellite according to the pre-stored satellite dynamic mathematical model, initial control force information and initial control moment information, and stores the orbit parameter information and attitude Quaternion information is sent to the sensor simulator.

[0036] Wherein, the satellite dynamics mathematical model includes a satellite attitude dynamics model and a sa...

Embodiment 2

[0060] The difference between this embodiment and Embodiment 1 is that in the satellite flight control closed-loop simulation system based on the component simulator provided by this embodiment, the sensor simulator includes: a sensor simulation server and a sensor data interface converter. The data interface converter connects the sensor simulation server and the onboard computer, and the sensor data interface converter is used to convert the data format of the communication between the sensor simulation server and the onboard computer; and the actuator simulator includes: the actuator simulation server and the actuator The data interface converter connects the actuator simulation server and the onboard computer through the actuator data interface converter, and the actuator data interface converter is used to convert the data format of the communication between the actuator simulation server and the onboard computer.

[0061] Further, in the existing actual satellite system, ...

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Abstract

The invention provides a satellite flight control closed loop simulation system based on a component simulator, which is applied to a system comprising a dynamics simulation server, a sensor simulator, an actuator simulator and a space-borne computer, wherein the formula of data output by the sensor simulator to the space-borne computer is the same as that of data output by a practical sensor to the space-borne computer, and the format of data received by the actuator simulator from the space-borne computer, i.e., the format of data input by an actuator is the same as that of data input by a practical actuator, so that the simulation reliability of the satellite flight control closed loop simulation system can be enhanced effectively; the component simulator is adopted instead of a real physical device, so that the simulation system has the advantages of low cost and low complexity; and meanwhile, the simulation system has the characteristics of high generality, high flexibility and high automatic degree, so that the research period of a satellite can be shortened effectively, and the research cost of the satellite is reduced.

Description

technical field [0001] The invention belongs to the technical field of satellite simulation testing, in particular to a satellite flight control closed-loop simulation system based on component simulators. Background technique [0002] In the field of aerospace engineering, due to the high cost of satellite development and the complex and harsh operating environment of satellites, it is generally necessary to simulate the flight control system of the satellite to verify the correctness of the design of the flight control system of the satellite. And test the function and performance of the satellite's flight control system. [0003] Usually, the flight control simulation system of the satellite can adopt semi-physical simulation and full-physical simulation. Among them, in the all-physical simulation system, since various real physical devices are directly connected to the simulation loop, the influence of these real physical devices on the performance of the simulation con...

Claims

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Application Information

Patent Timeline
11 Apr 2012
Publication
CN102411313A
IPC
G05B17/02
Inventors
张育林; 王兆魁