Abstract
This paper deals with the application of a linear parameter varying (LPV) controller synthesis for a modern air defense missile model. The model represents a challenging control problem due to the wide operation range. First, an LPV model of the missile is constructed via a novel approach of function substitution. Then, an LPV controller is designed based on the induced L2-norm framework. A mixed sensitivity weighting scheme is applied to specify the performance requirements. In order to fulfill various time and frequency domain criteria, a multiobjective optimization is used to tune the weighting functions of the mixed sensitivity weighting scheme. Finally, the robustness and performance of the controller is evaluated by nonlinear simulations.
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Tekin, R., Pfifer, H. (2013). Linear Parameter Varying Control of an Agile Missile Model Based on the Induced L 2-norm Framework. In: Chu, Q., Mulder, B., Choukroun, D., van Kampen, EJ., de Visser, C., Looye, G. (eds) Advances in Aerospace Guidance, Navigation and Control. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-38253-6_1
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DOI: https://doi.org/10.1007/978-3-642-38253-6_1
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-38252-9
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