制导火箭弹制导控制系统精益设计方法

制导火箭弹在陆军未来战争中正发挥越来越重要的作用,制导控制系统设计是制导火箭弹研制的核心和难题。提出了一种适用于制导火箭弹制导控制系统的精益设计方法,将设计过程分为数据处理环节、自动驾驶仪设计环节、制导律设计环节和六自由度仿真分析环节4个部分,并将标准化和基于模型的思想体现在精益化设计软件中,从而给出了一条可以又快又好地完成系统设计的技术途径。

A Lean Design Method of Guidance and Control System for Guided Rockets

Guided rockets are playing an increasingly important role in the army''s future war. The design of the guidance and control system is the core problem for the research of guided rockets. This paper proposes a lean design method for the guidance and control system of the guided rockets, and divides the design process into four parts: data processing, autopilot design, guidance law design and six-degree-of-freedom simulation analysis with standardization and model-based idea embodied in lean design software, which gives a technical way to complete system design quickly and well.