再入飞行器导航和制导系统的快速原型设计

Yongfeng Xie, Shuo Tang
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摘要

本文提出并实现了再入飞行器导航制导系统的快速原型设计方法。提出了基于快速控制原型的v循环开发方法,以实现导航制导系统的高效开发。V-Cycle方法中使用的高级建模和仿真工具以及RT-LAB等集成快速原型系统,与传统的开发方法相比,可以大大缩短导航制导系统的开发周期和成本。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Rapid prototyping of reentry vehicle navigation and guidance systems
In this paper, rapid prototyping method is proposed and implemented for the development of reentry vehicle navigation and guidance systems. V-Cycle development approach based on rapid control prototyping is introduced to develop navigation and guidance systems efficiently. High-level modeling and simulation tools and integrated rapid prototyping systems such as RT-LAB used in the V-Cycle approach can greatly reduce the cycle and cost for the development of navigation and guidance systems compared with traditional development methods.
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