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

Authors :
Sheng, Y. I.
Jiang, W. A. N. G.
Pei, Pei
Yongjia, Zhou
Source :
International Journal of Aerospace Engineering; 8/5/2020, p1-12, 12p
Publication Year :
2020

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. [ABSTRACT FROM AUTHOR]

Details

Language :
English
ISSN :
16875966
Database :
Complementary Index
Journal :
International Journal of Aerospace Engineering
Publication Type :
Academic Journal
Accession number :
144947569
Full Text :
https://doi.org/10.1155/2020/1764510