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数学仿真是研究航天器姿态轨道控制系统常用的手段,目前常用人工编程的方式建模,花费时间长且软件的可读性、可维护性较差.提出一套基于组态建模的航天器姿态轨道控制仿真系统,该系统通用性强、可支持自动建模及代码生成.仿真实例表明,该系统模块化、自动化程度较高,大大提高了研究人员的工作效率.
Mathematical simulation is a commonly used method to study attitude control orbit control system of spacecraft. At present, it is often modeled by human programming, which takes a long time and the software is readable and has poor maintainability.A set of spacecraft based on configuration modeling Attitude orbit control simulation system, which is versatile and supports automatic modeling and code generation.The simulation results show that the system is highly modular and highly automated, which greatly improves the work efficiency of researchers.