摘要
为了实现巡飞弹稳定飞行,提出了利用终端自适应滑模控制方式,将巡飞弹法向过载作为控制对象进行反馈控制;推导出控制器即舵偏角表达式,计算控制参数,使系统保持稳定,进行系统仿真,在存在扰动的情况下,检测系统的抗干扰能力;结果表明:终端自适应滑模控制系统可有效快速跟踪巡飞弹法向过载,具有很好的鲁棒性;为巡飞弹飞行控制系统研究提供依据和参考。
In order to achieve the stability of cruise missile flight,this paper put forward the method of terminal adaptive sliding mode control to make the normal overload of cruise missile as the control object for feedback control. We derived that controller is rudder angle expressions and calculated control parameter to make the system stable,and then simulated the system and detected the anti-interference ability of the system in the presence of disturbance. The terminal adaptive sliding mode control system could effectively fast track cruise missile normal overload which had the very good robustness. It could provide a basis and reference for the study of the cruise missile flight control system.
出处
《兵器装备工程学报》
CAS
2016年第11期35-39,共5页
Journal of Ordnance Equipment Engineering
关键词
巡飞弹
终端自适应
滑模控制
法向过载
cruise missile
terminal adaptive
sliding mode control
normal overload
