Abstract
This paper considers an adaptive output feedback fault tolerant control (FTC) for a reusable launch vehicle (RLV) during reentry phase for which four grid fins are used as actuators. Based on a prescribed tracking performance and an auxiliary system to deal with the input constraints, the proposed adaptive controller can compensate for the effect of uncertainties, external and internal disturbances, input constraints and actuator faults. It is shown that with the proposed scheme, the system tracking performance can be guaranteed even in the presence multiple actuator faults. The influence of the input constraints on the tracking performance is also investigated. Simulation results are presented to illustrate the effectiveness of the proposed scheme.
| Original language | English |
|---|---|
| Article number | 108616 |
| Journal | Aerospace Science and Technology |
| Volume | 142 |
| DOIs | |
| State | Published - Nov 2023 |
Keywords
- Backstepping control
- Fault tolerant control
- Prescribed transient
- Reusable launch vehicle
- Steady state performance
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