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Dual super-real-time rapid simulation test system and method applied to control system

A technology for control system and simulation testing, applied in general control systems, control/regulation systems, testing/monitoring control systems, etc. performance requirements, high simulation accuracy, and strong universality

Active Publication Date: 2020-07-03
SHANGHAI AEROSPACE CONTROL TECH INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] 1) The on-board computer running in the super-real-time system and the simulation step of the dynamic model are run in series, and the super-real-time acceleration rate is low
[0006] 2) Single super real-time mode
For long-period tasks, the simulation time is too long, time-consuming and labor-intensive

Method used

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  • Dual super-real-time rapid simulation test system and method applied to control system
  • Dual super-real-time rapid simulation test system and method applied to control system
  • Dual super-real-time rapid simulation test system and method applied to control system

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Embodiment Construction

[0054] The present invention will be described in detail below in conjunction with the accompanying drawings and examples.

[0055] Such as figure 1 As shown, the system of the present invention includes four components of a virtual computer, a dynamic model, a data bus and a co-simulation module, and is a dual ultra-real-time simulation testing system. Double super real-time includes hardware super real-time and software super real-time. The hardware super-real-time is to virtualize the on-board computer, simulate the on-board software operating environment in the equipment separated from the on-board product, and carry out information through the data bus and real-time dynamic model. (control signals and measurement information) interaction.

[0056] The on-board software acts as the controller in the control loop to output control signals, and the control signals are input into the dynamic model through the bus, and the actuators in the dynamic model respond to the control s...

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Abstract

The invention relates to a dual super-real-time rapid simulation test system and method applied to a control system. According to the characteristics of an in-orbit autonomous navigation guidance taskand the requirement of the in-orbit autonomous navigation guidance task on simulation rapidity, the invention provides the dual super-real-time rapid simulation test system applied to the control system. Simulation of a hardware super-real-time and software super-real-time dual super-real-time nesting mode is realized through a virtual computer, a dynamic model, a data bus and a collaborative simulation module, hardware is super-real-time and is oriented to GNC system closed loop simulation of the whole task process, universality is high, and simulation precision is high; software is super-real-time and is oriented to rapid state recursion of a task free operation stage, and the simulation acceleration ratio is high. The method is advantaged in that two modes can be integrated, the two super-real-time modes are coordinated and used in cooperation in the simulation process, the simulation process can be effectively accelerated, and the test rapidity requirement is met.

Description

technical field [0001] The invention relates to a fast simulation test technology of a satellite control system, which uses two super real-time nested fast simulation test methods: hardware super real-time and software super real-time. Background technique [0002] Commonly used test methods for satellite control system testing include: real-time simulation and semi-physical simulation. This type of simulation test method needs to run the on-board software on a real on-board computer. Limited by hardware conditions, this type of simulation test method can only be tested according to the real-time step size, and the simulation of long-period tasks is time-consuming and labor-intensive. [0003] The ultra-real-time simulation test uses virtual computer technology, and the on-board software runs in the on-board computer environment simulated by the test equipment, which can make the simulation time (the internal running time of the tested system) longer than the simulation time...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B23/02
CPCG05B23/0245Y02P90/02
Inventor 陈银河张小伟王静吉向坤戴维宗孟其琛张朝兴黄京梅刘笑梁巨平
Owner SHANGHAI AEROSPACE CONTROL TECH INST