Abstract:This paper is the result of a Master Thesis project performed at Saab AB. The main goal of the project was to design and implement a discrete time L 1 adaptive backup controller in pitch to increase performance for an agile fighter aircraft. A lateral controller was also developed as a secondary goal. A discrete time version of the Modified Piecewise Constant L 1 adaptive control formulation was implemented. Results have shown that augmenting a state-feedback controller with an L 1 adaptive controller increase… Show more
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