Three-dimensional impact angle constrained distributed cooperative guidance law for anti-ship missiles

• 来源期刊: 系统工程与电子技术（英文版）
• 年，卷（期）: 2021,（2）
• 所属期刊栏目: CONTROL THEORY AND APPLICATION
• 页码范围: 447-459
• 页数: 13页
• 语种: 英文
• DOI: 10.23919/JSEE.2021.000038

摘要

This paper investigates the problem of distributed co-operative guidance law design for multiple anti-ship missiles in the three-dimensional (3-D) space hitting simultaneously the same target with considering the desired terminal impact angle constraint. To address this issue, the problem formulation in-cluding 3-D nonlinear mathematical model description, and communication topology are built firstly. Then the consensus variable is constructed using the available information and can reach consensus under the proposed acceleration command along the line-of-sight (LOS) which satisfies the impact time con-straint. However, the normal accelerations are designed to gua-rantee the convergence of the LOS angular rate. Furthermore, consider the terminal impact angle constraints, a nonsingular terminal sliding mode (NTSM) control is introduced, and a finite time convergent control law of normal acceleration is proposed. The convergence of the proposed guidance law is proved by us-ing the second Lyapunov stability method, and numerical simu-lations are also conducted to verify its effectiveness. The results indicate that the proposed cooperative guidance law can regu-late the impact time error and impact angle error in finite time if the connecting time of the communication topology is longer than the required convergent time.