Abstract
Based on a gyroplane T-S fuzzy model in whole flight envelope, the equivalent control law, which is dependent on a set of available feedback control law parameters, is implemented using parameter robust design method according to the design requirements and the constraints of measurable states, sliding manifold parameters of the system is confirmed correspondingly, and the sliding mode control law, designed for the unmanned gyroplane in whole flight envelope, is realized. The simulation result shows that the system satisfies the dynamic performance with strong anti-interference ability, and the design method is feasible and effective.
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Lu, J., Chen, W. (2012). Robust Sliding Mode Control Law Design for Unmanned Gyroplane. In: Su, CY., Rakheja, S., Liu, H. (eds) Intelligent Robotics and Applications. ICIRA 2012. Lecture Notes in Computer Science(), vol 7506. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-33509-9_28
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DOI: https://doi.org/10.1007/978-3-642-33509-9_28
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-33508-2
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