摘要
针对多枚导弹打击同一目标的问题,进行协同制导律的设计。采用了能实现有限时间收敛的终端滑模控制法,既能满足攻击时间约束,又能实现期望的末端角度,并用李雅普诺夫稳定性理论证明了所得到的结果。最后通过仿真验证了提出的制导律的有效性。
In this paper, a missile cooperative guidance law was designed to solve the problem of multiple missiles hit ring the same target. With the terminal angle and impact time as constraints, a finite time convergence sliding mode control method was used to obtain the missile guidance law. The obtained result was proved by Lyapunov stability theory. A simulation was conducted and the results verified the effectiveness of the proposed method.
作者
杨其伟
王向华
YANG Qiwei WANG Xianghua(College of Electrical Engineering and Automation,Shandong University of Science and Technology, Qingdao, Shandong 266590, Chin)
出处
《山东科技大学学报(自然科学版)》
CAS
2017年第4期80-86,共7页
Journal of Shandong University of Science and Technology(Natural Science)
基金
青岛市博士后应用研究项目(2015179)
山东省博士后创新项目
山东科技大学研究生科技创新项目(SDKDYC170354)