Abstract
This paper designs a finite-time output tracking controller for air-breathing hypersonic vehicles (AHVs) subjected to disturbances and actuator constraints. After proper derivations, the original model is divided into two independent subsystems undergoing mismatched lumped disturbance. A finite-time disturbance observer (FTDO) is employed to estimate the lumped disturbance, while an auxiliary system combined with a command pre-filter is designed to analyze the effect of input saturation caused by the restrained actuators. Based on the FTDO and the auxiliary system, a novel integral sliding surface is constructed and then a chattering-free nonsingular controller is developed to realize finite-time output tracking in spite of mismatched lumped disturbance and input saturation, which is its major merit compared with other existing AHV controllers. A simulation study is carried out to verify the proposed control scheme.
| Original language | English |
|---|---|
| Pages (from-to) | 2578-2593 |
| Number of pages | 16 |
| Journal | Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering |
| Volume | 231 |
| Issue number | 14 |
| DOIs | |
| State | Published - 1 Dec 2017 |
Keywords
- Air-breathing hypersonic vehicles (AHVs)
- feedback linearization
- finite-time tracking
- input saturation
- nonsingularity and free-chattering
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