基于组态建模的航天器姿轨控数学仿真系统

A Configuration Modeling-Based Mathematic Simulation System for Spacecraft Attitude and Orbit Control

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.

Mathematic simulation is a useful method in the design of spacecraft attitude and orbit control system.Traditionally,researchers establish mathematical model by manual work,which is time-consuming and of low readability and maintainability.A kind of spacecraft attitude and orbit control simulation system based on configuration modeling is proposed in this paper.This system has a high expansibility and usability,and supports automatic modeling and coding.Simulation indicates that the system achieves a high degree of modularization and automatization,and helps researchers to improve efficiency greatly.