| 83 | 0 | 11 |
| 下载次数 | 被引频次 | 阅读次数 |
根据姿态运动学模型,分析了现代制导的弹药,飞行速度远远高于传统导弹,因此一般都要求具有快速的动态响应特性,来实现系统输出快速跟踪预测制导指令期望值。用输入输出线性化可以有效地代数补偿非线性系统模型具有线性的传递关系。进行了仿真验证,验证了方法的可行性。
Abstract:This paper analyzes the modern guidance ammunition according to the attitude kinematics model. The flight speed of modern guidance ammunition is much higher than that of conventional missile. So it is generally required to have fast dynamic response characteristics which can achieve fast tracking of predictive guidance expectations of system output. With the input and output linearization, it is can effectively compensate the nonlinear system model with linear transfer relationship in an algebraic way. This paper carries on a simulated verification to verify the feasibility of the method.
[1]杨荣军,王良明,孙瑞生.基于反馈线性化的制导炮弹弹道控制系统设计[J].火力与指挥控制,2013,38(1):20-23.
[2]钱杏芳,林瑞雄,赵亚男.导弹飞行力学[M].北京:北京理工大学出版社.2012.
[3]Tsourdos A,Blumel A.Flight Control Design for a Missile:an Approximate Feedback Linearization Approach[C]//Proceedings of the 7th Mediterranean Conference on Control and Automation.Haifa,Israel,1999:593-602.
[4]陈罗婧,刘莉,于剑桥.双通道控制旋转导弹自动驾驶仪解耦控制研究[J].北京理工大学学报,2008,28(1):11-14.
[5]韩晶,王华.基于反馈线性化的二维弹道修正控制系统设计[J].弹道学报,2010,22(2):27-31.
基本信息:
中图分类号:TJ765
引用信息:
[1]翟文军.基于输入输出线性化方法的制导弹药姿态控制系统设计[J].装备制造技术,2015,No.241(01):125-127.
2015-01-15
2015-01-15