Abstract
Anti-disturbance, continuous fixed-time controller is designed for faulted airbreathing hypersonic vehicle, including a fast fixed-time integral sliding surface (FFIS), a continuous fixed-time super-twisting-like reaching law (CFSTL) and a uniformly convergent observer. Firstly, the model of a hypersonic vehicle is established. Secondly, an FFIS is designed based on a newly presented fast fixed-time high-order regulator (FFTR). Then, a CFSTL is applied to drive the sliding mode vector and its derivative to achieve fixed-time convergence. Finally, lumped disturbances are estimated by a uniformly convergent observer.
Keywords: Air-breathing hypersonic vehicle, Disturbance observer, Fixed-time control, Sliding mode control.
About this chapter
Cite this chapter as:
Yibo Ding, Wenbo Li, Panxing Huang, Jiashun Si, Fenglin Wang ;Anti-Disturbance Continuous Fixed-Time Controller Design for Air-breathing Hypersonic Vehicle, Advanced Control of Flight Vehicle Maneuver and Operation Frontiers in Aerospace Science (2023) 4: 1. https://doi.org/10.2174/9789815050028123040003
| DOI https://doi.org/10.2174/9789815050028123040003 |
Print ISSN 2468-4716 |
| Publisher Name Bentham Science Publisher |
Online ISSN 2468-4724 |

