A New United Proportional Navigation Guidance for Impact Angle Constraint without Measurement Distance between Vehicle and Target

Author:

Yang Hao1ORCID,Wu Hangjin1ORCID,Bai Xibin1ORCID,Zhang Shifeng1ORCID

Affiliation:

1. College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China

Abstract

This paper proposed a united proportional navigation guidance (UPNG) method to alleviate the guidance command saltation with an impact angle constraint under the condition of no real-time distance between the vehicle and the target (line-of-sight (LOS) distance). Firstly, based on the biased proportional navigation guidance (BPNG), a smooth-biased proportional navigation guidance (SBPNG) method was proposed, whose bias term was designed as a trigonometric function. In SBPNG method, due to the continuous smooth change of the bias term, the guidance command would not saltus anymore, and the impact angle was controlled by the bias integral component. Secondly, biased on SBPNG method, the united proportional navigation guidance (UPNG) method combining SBPNG and variable coefficient proportional navigation guidance (VCPNG) was established. In UPNG method, because there was no LOS distance, the guidance coefficient was designed as a function of the difference between the expected impact angle and the estimated impact angle, so the closed-loop control of impact angle was realized. Finally, a lot of simulation experiments on different guidance laws were carried out without real-time LOS distance. The results verify that the UPNG method proposed in this paper solves the problem of guidance command saltation effectively and has better robustness in impact angle control.

Funder

National Natural Science Foundation of China

Publisher

Hindawi Limited

Subject

Applied Mathematics,General Mathematics

Reference30 articles.

1. Lyapunov-Based Pursuit Guidance Law with Impact Angle Constraint

2. The development of radar homing missiles

3. Stability of spinning missile with homing proportional guidance law;X. Hu;Aerospace and Electronic Systems,2017

4. Visibility augmented proportional navigation guidance;G. Franzini;Journal of Guidance, Control, and Dynamics,2018

5. Impact Time Control Cooperative Guidance Law Design Based on Modified Proportional Navigation

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