二维弹道修正引信制动控制建模与仿真 |
| |
引用本文: | 卢志才,高敏,贾春宁.二维弹道修正引信制动控制建模与仿真[J].弹箭与制导学报,2016(2):97-101. |
| |
作者姓名: | 卢志才 高敏 贾春宁 |
| |
作者单位: | 1. 解放军军械工程学院,石家庄,050003;2. 总装驻上海地区军事代表室,上海,201109 |
| |
基金项目: | 武器装备预研基金;军械工程学院基金(YJJXM13020) |
| |
摘 要: | 为解决二维弹道修正引信滚转姿态实时控制问题,提出了固定舵制动模型。根据弹道修正原理及固定舵控制规律,建立了制动控制数学模型。构建了基于双轴仿真测试转台的半实物仿真系统,对不同弹道环境下制动控制性能进行了半实物仿真。结果表明干扰力矩在0~0.5 N · m变化范围,该方法能够有效跟踪滚转角控制指令实现实时跟踪。当弹丸转速在100~167 r/s范围时,该模型制动时间和精度满足控制系统总体要求。
|
关 键 词: | 固定舵 半实物仿真 制动控制 直流电机 二维弹道修正引信 |
Braking Control Model and Simulation for Precision Guided Kit |
| |
Abstract: | To solve roll attitude real-time control problem for a 155 mm canard guided dual-spin stabilized projectiles , braking control model was proposed .According to trajectory correction theory and canards braking principle , the trajectory braking control model was given .The semi-physical simulation system was set up based on tow-axis flight simulation table , which can drive the dual-spin stabilized projectiles at different roll rate.The results show that braking model can rack roll attitude control-instruction under condition of 0.5 N· m disturb mo-ment , and the nose portion can brake accurately at control roll attitude when the projectiles rotate at 100 r/s to 167 r/s.The braking preci-sion and duration time can fulfill the need of guidance and control system . |
| |
Keywords: | fixed canards semi-physical simulation braking control precision guided kit |
本文献已被 万方数据 等数据库收录! |