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Semi-physical simulation synchronization evaluation system and method for launch vehicle control system

A semi-physical simulation and control system technology, applied in general control systems, control/adjustment systems, electrical testing/monitoring, etc., can solve problems such as threats, damage to test equipment, and difficulty in judging problem nodes, and achieve the effect of avoiding damage

Active Publication Date: 2017-05-24
SHANGHAI AEROSPACE CONTROL TECH INST
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AI Technical Summary

Problems solved by technology

Since the hardware-in-the-loop simulation is a closed-loop simulation, this method cannot detect abnormal data in each link of the hardware-in-the-loop simulation in real time, which makes it difficult to judge the problem node
The semi-physical simulation test equipment includes large-scale test equipment such as three-axis turntables and rocket engines. Data divergence cannot be detected in time during the test, which will cause damage to the test equipment. Problems such as "speeding" of the turntable may also pose a threat to the safety of test personnel.

Method used

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  • Semi-physical simulation synchronization evaluation system and method for launch vehicle control system
  • Semi-physical simulation synchronization evaluation system and method for launch vehicle control system
  • Semi-physical simulation synchronization evaluation system and method for launch vehicle control system

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Embodiment Construction

[0026] The present invention will be further elaborated below by describing a preferred specific embodiment in detail in conjunction with the accompanying drawings.

[0027] like figure 1 As shown, a hardware-in-the-loop simulation synchronous evaluation system for a launch vehicle control system includes: a hardware-in-the-loop simulation system 1 for outputting real engine swing angle information; a synchronization simulation system 2 for generating pendulum angle information according to the real engine swing angle Angle control command; data acquisition and monitoring system 3, its input end is respectively connected with hardware-in-the-loop simulation system and synchronous simulation system. The real engine swing angle measurement information of the semi-physical simulation is connected to the synchronous mathematical simulation system through the A / D interface; the output signals of each link of the semi-physical simulation system 1 (including the output signal of the ...

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Abstract

The invention discloses a semi-physical simulation synchronization evaluation system and method for a launch vehicle control system. The method comprises: S1, when a semi-physical simulation system is used for carrying out semi-physical simulation of a launch vehicle control system, a synchronization simulation system carries out mathematic simulation, output data of all links of semi-physical simulation and mathematic simulation are compared in real time, and the operation situation of the semi-physical simulation system is evaluated in real time based on the deviation situation of the output data to control operation or stopping of the simulation process; and S2, after testing, the output data of all links of semi-physical simulation and mathematical simulation during the whole period are analyzed to realize evaluation of the whole semi-physical simulation process. Therefore, real-time monitoring of the semi-physical simulation system can be realized; and reliability of the system can be improved.

Description

technical field [0001] The invention relates to the field of semi-physical simulation of a launch vehicle control system, in particular to a synchronous evaluation system and method for a semi-physical simulation of a launch vehicle control system. Background technique [0002] In the existing hardware-in-the-loop simulation system of the launch vehicle control system, a simulator is used to solve the link of the rocket body, and other links such as inertial groups, arrow machines and servo mechanisms are realized with real products. Usually, after the half-in-the-loop simulation test is completed, the test data and Mathematical simulation comparison to evaluate the effectiveness of hardware-in-the-loop simulation. Since the hardware-in-the-loop simulation is a closed-loop simulation, this method cannot detect abnormal data in each link of the hardware-in-the-loop simulation in real time, which makes it difficult to judge the problem node. The hardware-in-the-loop simulatio...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B17/02G05B23/02
Inventor 于亚男王迪余薛浩周静陈海朋胡存明
Owner SHANGHAI AEROSPACE CONTROL TECH INST
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