Flight Mode Transitions for a Fixed-Wing Mini Aerial Vehicle from/to Hovering

Myrand-Lapierre, Vincent; Desbiens, André; Gagnon, Éric; Wong, Frank; Poulin, Éric C.

doi:10.2514/6.2011-6402

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2015

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“…8 A logic-based supervisor has been designed to manage the switching moments between two main controllers. 9 Inverse dynamics has generated the trajectory for transition from vertical takeoff and landing (VTOL) to wing-borne flight. 10 A class of ''policy holding'' strategies have been proposed in the presence of measurement noise in Garone et al…”

Section: Introductionmentioning

confidence: 99%

Design of adaptive switching control for hypersonic aircraft

Jiao

Jiang

2015

Advances in Mechanical Engineering

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This article proposes a novel adaptive switching control of hypersonic aircraft based on type-2 Takagi-Sugeno-Kang fuzzy sliding mode control and focuses on the problem of stability and smoothness in the switching process. This method uses full-state feedback to linearize the nonlinear model of hypersonic aircraft. Combining the interval type-2 TakagiSugeno-Kang fuzzy approach with sliding mode control keeps the adaptive switching process stable and smooth. For rapid stabilization of the system, the adaptive laws use a direct constructive Lyapunov analysis together with an established type-2 Takagi-Sugeno-Kang fuzzy logic system. Simulation results indicate that the proposed control scheme can maintain the stability and smoothness of switching process for the hypersonic aircraft.

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Section: Introductionmentioning

confidence: 99%