STM32导弹助推器推力矢量控制回路设计

摘要本文内容主要包括，垂直发射推力矢量问题建模和分析，转弯程序优化设计以及软硬件模拟平台搭建。选用扰流片推力控制，建立导弹751自由度方程和推导纵向的扰动方程。搭建转弯控制回路，以粒子群算法与遗传算法结合的方法优化推力矢量的转弯指令。选用STM32系列微控制器设计硬件控制板，基于μC/OS-II操作系统和μC/GUI图形系统环境，实现无线指令传递、用户界面设计和数模转换等功能。实现一套由计算机确定指令，硬件控制板接收并处理信号，4-20mA电流信号经放大器控制比例电磁阀开度的装置，模拟扰流片经液压驱动改变遮蔽喷管口的深度产生转弯控制气动力的过程。30454
关键词推力矢量转弯控制优化 STM32
毕业论文设计说明书外文摘要
Title Design and simulation of a missile booster thrust
vector control loop
Abstract
This paper is on the design of thrust vector control with the spoiler system for vertical launching .Based on the spoiler, missile model with six degrees of freedom was designed using Simulink computational method，and Mathematical model of longitudinal disturbance in the loop for turning control was derived and conducted with frequency domain analysis. To get the feasible vertical launch turning law, a optimization algorithm which combines PSO with GA was employed to seek.
Then, a hardware control panel using the stm32 mcu was to realize some functions, such as wireless command signal transmission, user interface, digital to analog conversion and so on. To ensure the real-time performance, the software development environment on this chip board is based on μC/OS-II operating system and μC/GUI graphics system. The control panel receives the command signals of turning angle of the spoiler, and pass the current signal of 4-20mA to drive a proportional solenoid valve through a amplifier. The opening degree of Proportional solenoid valve cause The motion of spoiler which produces aerodynamic for turn control.
Keywords vertical launch turning control optimization algorithm STM32
目次
1    绪论    1
1.1 垂直发射    1
1.2 推力矢量    3
1.3 垂直发射转弯控制    4
1.4 本课题研究方向    5
2    垂直发射模型    6
2.1 扰流片    6
2.2 导弹751自由度数学模型    7
2.3 导弹纵向短周期扰动模型    11
2.4 导弹751自由度SIMULINK建模    14
2.5 垂直发射控制回路    17
2.6 本章小结    18
3    垂直发射转弯优化设计    19
3.1 算法    19
3.2 优化问题    23
3.3 MATLAB优化寻解    25
3.4 本章小结    28
4    控制板硬件设计与制作    29
4.1 整体设计思路    29
4.2 硬件器件的选择    29
4.3 硬件设计框图    32
4.4 硬件模块化原理图设计    32
4.5 硬件PCB制作    36
4.6 本章小结    38
5    控制板软件设计    39
5.1 设计思路    39
5.2 软件设计环境    39
5.3 软件模块化设计    40
5.4 本章小结    43
6    控制台程序设计    45 STM32导弹助推器推力矢量控制回路设计:http://www.751com.cn/jixie/lunwen_26164.html