Prescribed-Time Chattering-Free Sliding Mode Guidance Law With Terminal Angle Constraint Based on Periodic Delayed Feedback
This article proposes a prescribed-time chattering-free sliding mode guidance law with terminal angle constraint based on periodic delayed feedback. First, a prescribed-time sliding mode guidance law is presented based on a periodic delayed sliding mode surface, which can ensure the prescribed-time convergence of both the line-of-sight angular rate and the line-of-sight angle. Second, a prescribed-time extended state observer is proposed to acquire the precise disturbance estimation within the prescribed settling time. In contrast to other finite-time or fixed-time disturbance observer, the convergence time of the proposed observer is concise and easy for tuning. Finally, by incorporating the estimated disturbance into the original prescribed-time sliding mode guidance law, a composite guidance law with prescribed-time convergence is developed, where chattering is completely eliminated. In particular, the convergence time of the proposed prescribed-time extended state observer and prescribed-time sliding mode guidance law can be arbitrarily assigned and prescribed in advance. A series of numerical simulations are carried out to verify the efficacy of the proposed guidance law.
Authors
- Bin Zhou (ORCID: https://orcid.org/0000-0003-1272-2652)
- Yi Ding (ORCID: https://orcid.org/0000-0003-4389-5636)
- Mingrui Hao
- Haoyu Zheng
Institutions
- Harbin Institute of Technology (CN)
Publication Details
- Journal
- IEEE Transactions on Aerospace and Electronic Systems
- Published
- 2024-08-26
- DOI
- https://doi.org/10.1109/taes.2024.3449274
- Citations
- 5
- Primary Topic
- Bladed Disk Vibration Dynamics
- Type
- article
- Field-Weighted Citation Impact
- 1.30
Funders
- Fundamental Research Funds for the Central Universities