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