Abstract
Among flourishing control studies on air-breathing hypersonic vehicles (AHVs), actuator characteristics have not been fully accommodated. This study gives a comprehensive consideration to physical actuators of AHVs that have transient dynamics and magnitude/rate constraints by introducing an adaptive reference governor and an optimizing allocation module. After implementing a tangent tracking error-based back-stepping design, the derived control algorithm is low-complexity, whose effectiveness is verified by simulations.
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