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Design and realization of the high accuracy attitude and orbit control real-time simulation platform for spacecraft

机译:宇宙飞船高精度姿态和轨道控制实时仿真平台的设计与实现

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摘要

To verify the correctness and real-time performance of the high accuracy attitude and orbit control algorithms for spacecraft mission, the attitude and orbit control software is developed based on the embedded real-time VxWorks operation system, and based on the high accuracy attitude and orbit dynamic simulation software, aground real-time simulation platform is established. The software as well as hardware architecture and interface of the simulation platform are introduced. The key problems are solved, including the synchronization and data communication between the onboard computer and the dynamic simulation computer, and the wireless communication between the on-board computer and the ground control center. The simulation result shows that reliability and real time of the platform can meet the requirements, and the platform provides a good support environment for the attitude and orbit control ground test and performance evaluation for spacecrafts.
机译:为了验证航天器任务的高精度姿态和轨道控制算法的正确性和实时性能,态度和轨道控制软件是基于嵌入式实时VxWorks操作系统开发的,并基于高精度姿态和轨道 动态仿真软件,建立了搁浅的实时仿真平台。 介绍了软件以及仿真平台的硬件架构和接口。 解决了关键问题,包括板载计算机与动态仿真计算机之间的同步和数据通信,以及车载计算机和地面控制中心之间的无线通信。 仿真结果表明,平台的可靠性和实时可以满足要求,平台为态度和轨道控制地面测试和宇宙飞船进行性能评估提供了良好的支持环境。

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