[1]何阳光,李小兵,赵思源,等.弹性体导弹自适应减振跟踪控制算法[J].ag亚游ag8|官方,2019,41(03):97.[doi:.]
 HE Yangguang,LI Xiaobing,ZHAO Siyuan,et al.Adaptive Damping Tracking Control for Elastic Missile[J].,2019,41(03):97.[doi:.]
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弹性体导弹自适应减振跟踪控制算法()
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《ag亚游ag8|官方》[ISSN:1008-1194/CN:61-1316/TJ]

卷:
41
期数:
2019年03
页码:
97
栏目:
出版日期:
2019-06-24

文章信息/Info

Title:
Adaptive Damping Tracking Control for Elastic Missile
文章编号:
1008-1194(2019)03-0097-07
作者:
何阳光;?李小兵;?赵思源;?熊思宇
空军工程大学防空反导学院,陕西 西安 710051
Author(s):
HE Yangguang;?LI Xiaobing;?ZHAO Siyuan;?XIONG Siyu
Air and Missile Defense College,Air Force Engineering University,Xi’an 710051,China
关键词:
干扰观测器;?自适应;?滤波;?弹性振动
Keywords:
disturbance observer;?adaptive;?filter;?elastic vibration
分类号:
TJ760
DOI:
.
文献标志码:
A
摘要:
针对现有控制方法难以克服弹性体导弹弹性振动与刚体运动耦合问题,提出一种基于非线性干扰观测器的自适应反演控制算法。该算法能够根据弹体振动的强度动态调整控制器增益,提高不同情况下的控制性能,保证系统的稳定性。仿真结果表明,所提出的控制算法能够有效抑制弹性振动的耦合影响,并实现导弹姿态的稳定跟踪。
Abstract:
An adaptive backstepping controller based on nonlinear disturbance observer was proposed for the elastic missile with elastic vibration and rigid body motion coupling. The method could adjust the controller gain dynamically according to the vibration intensity of the missile body, improved the control performance under different conditions and ensured the stability of the system. The simulation results showeded that the controller could effectively suppress the influence of elastic vibration and achieved stable tracking of missile attitude.

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备注/Memo

备注/Memo:
收稿日期:2018-12-06
基金项目:国家自然科学基金项目资助(61603410)
作者简介:何阳光(1993—),男,河南周口人,硕士研究生,研究方向:弹性体导弹控制。E-mail:1780955773@qq.com。
更新日期/Last Update: 2019-07-11