Abstract

The implementation of advanced guidance laws with bearings-only measurements requires estimation of the range information. To improve estimation accuracy and satisfy the impact angle constraint, this paper proposes a two-phase optimal guidance law consisting of an observing phase and an attacking phase. In the observing phase, the determinant of Fisher information matrix is maximized to achieve the optimal observability and a suboptimal solution expressed by leading angle is derived analytically. Then, a terminal sliding-mode guidance law is designed to track the desired leading angle. In the followed attacking phase, an optimal guidance law is integrated with a switching term to satisfy both the impact angle constraint and the field-of-view constraint. Finally, comparison studies of the proposed guidance law and a traditional optimal guidance law are conducted on stationary targets and maneuvering targets cases. Simulation results demonstrate that the proposed guidance law is able to improve the range observability and achieve better terminal performances including impact angle accuracy and miss distance.

Highlights

  • Research on impact angle constrained guidance laws can be divided into two categories, that is, augmented proportional navigation (APN) guidance laws and advanced guidance laws

  • Different filters including extended Kalman filter (EKF) [9], particle filter (PF) [10, 11], maximum likelihood estimation (MLE), [12] and pseudo-linear estimation [13] were successfully applied in bearings-only target motion analysis (TMA)

  • The median value of impact angle errors obtained by TPOGL is 0.91∘ while that obtained by optimal guidance law (OGL) is 3.81∘, and TPOGL improves the accuracy by 76%

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Summary

Introduction

Research on impact angle constrained guidance laws can be divided into two categories, that is, augmented proportional navigation (APN) guidance laws and advanced guidance laws. APN guidance laws can achieve the desired impact angle with only information of line-of-sight (LOS) angle or LOS angular rate by adjusting the proportional navigation coefficient [1] or adding a bias term [2, 3]. It is always assumed in APN approaches that the target is stationary or the target’s maneuvering path is known. To trade off the requirements of observability enhancement and impact angle constraint, this paper proposes a two-phase optimal guidance law (denoted as TPOGL). The proposed TPOGL has a simple structure and can be implemented in real time

Problem Statement
Two-Phase Optimal Guidance Law Design
Simulation
Findings
Conclusion
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