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Linear Parameter Varying Versus Linear Time Invariant Reduced Order Controller Design of Turboprop Aircraft Dynamics
Widowati1, Bambang Riyanto2 & Hari Muhammad3
1Mathematics Department, Diponegoro University
Jl. Prof. H. Soedarto, S.H., Semarang, 50275, Indonesia
2Electrical Engineering Study Program, Institut Teknologi Bandung
Jl. Ganesha No. 10 Bandung, 40132, Indonesia
3Aerospace Engineering Study Program, Institut Teknologi Bandung
E-mail: widowati_math@undip.ac.id
Abstract. The applicability of parameter varying reduced order controllers to aircraft model is proposed. The generalization of the balanced singular perturbation method of linear time invariant (LTI) system is used to reduce the order of linear parameter varying (LPV) system. Based on the reduced order model the low-order LPV controller is designed by using synthesis technique. The performance of the reduced order controller is examined by applying it to lateral-directional control of aircraft model having 20th order. Furthermore, the time responses of the closed loop system with reduced order LPV controllers and reduced order LTI controller is compared. From the simulation results, the 8th order LPV controller can maintain stability and to provide the same level of closed-loop systems performance as the full-order LPV controller. It is different with the reduced-order LTI controller that cannot maintain stability and performance for all allowable parameter trajectories.
Keywords: synthesis; singular perturbation approximation; reduced-order LPV controller; stability; aircraft dynamics.
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