Optimal three-dimensional impact time guidance with seeker's field-of-view constraint

• 来源期刊: 中国航空学报（英文版）
• 年，卷（期）: 2021,（2）
• 页码范围: 240-251
• 页数: 12页
• 语种: 英文

摘要

This paper proposes a new three-dimensional optimal guidance law for impact time con-trol with seeker's Field-of-View (FOV) constraint to intercept a stationary target. The proposed guidance law is devised in conjunction with the concept of biased Proportional Navigation Guid-ance (PNG). The guidance law developed leverages a nonlinear function to ensure the boundedness of velocity lead angle to cater to the seeker's FOV limit. It is proven that the impact time error is nullified in a finite-time under the proposed method. Additionally, the optimality of the biased com-mand is theoretically analyzed. Numerical simulations confirm the superiority of the proposed method and validate the analytic findings.