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Information Journal Paper

Title

Stabilization of the F-8 Fighter Aircraft Using Model-Based Predictive Control

Pages

  1-15

Abstract

 The aircraft stabilizer stabilizes the aircraft utilizing non-fixed and controllable aerodynamic surfaces. This paper presents a Model-Based Predictive Control for F-8 Fighter Aircraft Stabilization. In the proposed control method, meanwhile the real-time optimization, the cost-function is minimized by means of the linearized model of F-8 fighter and the output is predicted in future interval times based on the Receding horizon strategy. The cost-function is defined as the aggregate of terminal cost and summation of stage costs, that the quadratic form of cost-function is utilized in control algorithm, eventually. The costfunction minimization is giving rise to stable control input. The extracted stable control input stabilized the states of the nonlinear F-8 fighter system under the various initial conditions. The considerations are taken into account in the controller designing steps, to reduce the computational load. Mathematical proof investigates that the closed-loop system with the proposed control has asymptotic stability. The simulation results well demonstrate the favorable efficiency of the proposed controller in F-8 Fighter Aircraft Stabilization.

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  • Cite

    APA: Copy

    VEYSI, MOHAMMAD, SOLTANPOUR, MOHAMMAD REZA, & Khalilpour, Jafar. (2018). Stabilization of the F-8 Fighter Aircraft Using Model-Based Predictive Control. JOURNAL OF AERONAUTICAL ENGINEERING (JOAE), 20(2 ), 1-15. SID. https://sid.ir/paper/367857/en

    Vancouver: Copy

    VEYSI MOHAMMAD, SOLTANPOUR MOHAMMAD REZA, Khalilpour Jafar. Stabilization of the F-8 Fighter Aircraft Using Model-Based Predictive Control. JOURNAL OF AERONAUTICAL ENGINEERING (JOAE)[Internet]. 2018;20(2 ):1-15. Available from: https://sid.ir/paper/367857/en

    IEEE: Copy

    MOHAMMAD VEYSI, MOHAMMAD REZA SOLTANPOUR, and Jafar Khalilpour, “Stabilization of the F-8 Fighter Aircraft Using Model-Based Predictive Control,” JOURNAL OF AERONAUTICAL ENGINEERING (JOAE), vol. 20, no. 2 , pp. 1–15, 2018, [Online]. Available: https://sid.ir/paper/367857/en

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