A Switching Prescribed Performance Control Approach for Attitude Control of RLVs with Finite-Time Convergence
This paper presents the application of our recent published prescribed performance control theory, to the control of the attitude of a RLV during the landing approach. The proposed control solution offers the possibility to enforce the attitude error to belong to given prescribed bounds. Furthermore, it allows the attitude of the RLV, to reach its attitude’s reference in finite time. Parameters tuning of the control algorithm is also discussed. A simulation campaign conducted under a realistic flight environment (wind and atmospheric turbulence, uncertainties in the initial attitude of the vehicle), illustrates the potential of the proposed control approach.
Authors
- Jing Chang (ORCID: https://orcid.org/0000-0003-4103-9115)
- Alejandra Ferreira de Loza (ORCID: https://orcid.org/0000-0003-1189-0857)
- Jérôme Cieslak (ORCID: https://orcid.org/0000-0002-7166-1880)
- Zongyi Guo (ORCID: https://orcid.org/0000-0001-6837-9924)
- David Henry (ORCID: https://orcid.org/0000-0001-7169-7704)
Institutions
- Centre National de la Recherche Scientifique (FR)
- Xidian University (CN)
- Université de Bordeaux (FR)
- Northwestern Polytechnical University (CN)
- Laboratoire de l'Intégration du Matériau au Système (FR)
- Institut Polytechnique de Bordeaux (FR)
- Instituto Politécnico Nacional (MX)
Publication Details
- Journal
- IFAC-PapersOnLine
- Published
- 2025-01-01
- DOI
- https://doi.org/10.1016/j.ifacol.2025.11.116
- Primary Topic
- Adaptive Control of Nonlinear Systems
- Type
- article
- Field-Weighted Citation Impact
- 0.00