Discrete-Time Angle Constraint Interception with Model-Assisted Target Maneuver Estimator

Author:

Sheng Y. I.1,Jiang W. A. N. G.23ORCID,Pei Pei23ORCID,Yongjia Zhou4

Affiliation:

1. School of Mechatronical Engineering, Beijing Institute of Technology, Beijing 100081, China

2. School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China

3. Beijing Key laboratory of UAV Autonomous Control, Beijing Institute of Technology, Beijing 100081, China

4. Northwest Industries Group CO., LTD, Xian, 710000, China

Abstract

This paper investigates the problem of designing angle constraint guidance law against unknown maneuvering targets based on discrete-time sliding mode control theory. Invoking the fact that the future course of action of the target, an independent entity, cannot be predicted beforehand due to its complexity and unpredictability, a model-assisted discrete-time disturbance observer in cooperation with a singularity-free strategy is proposed first to estimate the target maneuver. Based on the reconstructed signal and a fast convergence time-varying sliding surface, a new chattering-mitigated super-twisting-like discrete-time impact angle constraint guidance law is then synthesized. Stability analysis shows that the closed-loop system trajectory can be forced to enter into a small region around the sliding surface. Simulations and comparisons with classical discrete-time sliding mode guidance law validate the effectiveness of the proposed guidance law.

Funder

National Natural Science Foundation of China

Publisher

Hindawi Limited

Subject

Aerospace Engineering

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