| 运载火箭姿态控制系统稳定性分析 |
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| 引用本文： | 丰晓霞,夏广庆,韩秀利,韩晓明.运载火箭姿态控制系统稳定性分析[J].大连理工大学学报,2015,55(5):542-547. |
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| 作者姓名： | 丰晓霞 夏广庆 韩秀利 韩晓明 |
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| 基金项目： | 国家自然科学基金资助项目(1120204411105023)；中国博士后科学基金资助项目(2013M541230). |
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| 摘 要： | 为解决无控刚性箭体和弹性箭体姿态控制系统的不稳定问题,以俯仰通道为例,对无控刚性箭体引入了姿态角偏差和姿态角速度偏差反馈,设计了PD控制器;对弹性箭体引入结构滤波器,进行控制器设计.仿真结果显示无控刚性箭体和弹性箭体姿态控制系统俯仰通道的稳态误差分别为0.05%、-0.30%,从而使无控刚性箭体和弹性箭体姿态控制系统的不稳定问题得到了有效控制.
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| 关 键 词： | 运载火箭 稳定性分析 PD控制器 结构滤波器 |
Analysis of stability for launch vehicle attitude control system |
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| FENG Xiaoxi,XIA Guangqing,HAN Xiuli,HAN Xiaoming.Analysis of stability for launch vehicle attitude control system[J].Journal of Dalian University of Technology,2015,55(5):542-547. |
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| Authors: | FENG Xiaoxi XIA Guangqing HAN Xiuli HAN Xiaoming |
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| Abstract: | In order to solve the instability of free rigid rocket and elastic rocket attitude control systems, taking the pitch channel as an example, the attitude angle and attitude angular velocity deviation feedbacks are added to the PD controller for the free rigid rocket, and a structure filter is added to the controller for the elastic rocket. The simulation results show that pitch channel steady-state errors of free rigid rocket and elastic rocket attitude control systems are 0.05%, -0.30% separately. So the instability of free rigid rocket and elastic rocket attitude control systems is controlled effectively. |
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| Keywords: | launch vehicle analysis of stability PD controller structure filter |
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