Adaptive Finite-Time Preassigned Performance Control for Hypersonic Vehicles with Lumped Perturbations
This paper proposes an adaptive finite-time preassigned performance control (PPC) approach to solve the attitude control problem of hypersonic vehicles (HSVs) suffering from lumped disturbances. A specific preassigned performance function guaranteeing finite-time stability and small overshoot is presented to constrain the attitude tracking errors. Moreover, a novel synchronous disturbance estimation is presented to build a disturbance observer (DO). Based on the devised preassigned performance function and the information from the DO, an adaptive finite-time preassigned performance controller is devised to solve the attitude control problem. Finally, numerical examples demonstrate the validity of the presented algorithm.
Authors
- Rugang Tang (ORCID: https://orcid.org/0000-0003-1572-1794)
- Zheng Wang (ORCID: https://orcid.org/0000-0002-4073-6923)
- Xin Ning (ORCID: https://orcid.org/0000-0003-3663-3996)
- Chengfeng Luo (ORCID: https://orcid.org/0000-0002-9426-1716)
Institutions
- Northwestern Polytechnical University (CN)
- Northwest Institute of Mechanical and Electrical Engineering (CN)
Publication Details
- Published
- 2024-12-12
- DOI
- https://doi.org/10.1109/icarcv63323.2024.10821624
- Citations
- 1
- Primary Topic
- Advanced Control Systems Optimization
- Type
- article
- Field-Weighted Citation Impact
- 0.33
Funders
- National Natural Science Foundation of China
- National Key Laboratory of Science and Technology on Communications