火力与指挥控制2018，Vol.43Issue(1)：165-168,174,5.DOI:10.3969/j.issn.1002-0640.2018.01.035
航天飞行器总体性能仿真验证系统设计与实现
Design and Implementation of Simulation System for Overall Performance of Spacecraft
李杰奇 1孔福 2李争学 1彭健1
作者信息
- 1. 中国运载火箭技术研究院,北京100076
- 2. 北京机电工程总体设计部,北京100854
- 折叠
摘要
Abstract
In order to reduce the development cost and improve the development efficiency, a set of reusable and extensible simulation system for semi - physical performance simulation is designed and analyzed by analyzing the characteristics and verification requirements of each stage of the space vehicle. The system integrates the system models of aircraft navigation / guidance / control, power supply and distribution, measurement and control communication, structural mechanism and control of reverse thrust.By using semi-physical test technology, virtual scene simulation technology and physical motion demonstration technology.Analysis and verification of the overall performance of large-scale integrated system and technical indicators. Simulation results show that the system is stable, reliable and feasible,and it can be used as a technical platform for the simulation and verification of the overall performance of the aircraft. The simulation verification system has been applied in many research models.关键词
航天飞行器/总体性能/仿真验证Key words
aerospace vehicles/overall performance/simulation verification system分类
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李杰奇,孔福,李争学,彭健..航天飞行器总体性能仿真验证系统设计与实现[J].火力与指挥控制,2018,43(1):165-168,174,5.
