Flight Parameter Analysis of an L1 Adaptive Controller of a Hypersonic Glider

What is it about?

The paper addresses a number of long-standing challenges of automatic control of hypersonic vehicles that exhibits numerous aerodynamic and structural uncertainties across extremely side Mach-Altitude flight envelope. The paper presents a full state feedback stabilising controller and to analyse the variability of the aerodynamic characteristics by utilising the estimator characteristics of the augmented L1 adaptive control architecture.

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