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Information Journal Paper

Title

NONLINEAR OPTIMAL CONTROL TECHNIQUES APPLIED TO A LAUNCH VEHICLE AUTOPILOT

Pages

  43-49

Keywords

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Abstract

 This paper presents an application of the nonlinear optimal control techniques to the design of launch vehicle autopilots. The optimal control is given by the solution to the Hamilton-Jacobi-Bellman (HJB) equation, which in this case cannot be solved explicity. A method based upon Successive Galerkin Approximation (SGA) is used to obtain an approximate optimal solution. Simulation results involving the three degrees-of-freedom (3DOF) model of a launch vehicle during atmospheric flight are reported to demonstrate the performance of the considered autopilot. Alternative results are also presented for classical and linear optimal approaches.

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    APA: Copy

    IRANI RAHAGHI, M., & ROSHANIAN, J.. (2006). NONLINEAR OPTIMAL CONTROL TECHNIQUES APPLIED TO A LAUNCH VEHICLE AUTOPILOT. JOURNAL OF AEROSPACE SCIENCE AND TECHNOLOGY (JAST), 3(1), 43-49. SID. https://sid.ir/paper/290935/en

    Vancouver: Copy

    IRANI RAHAGHI M., ROSHANIAN J.. NONLINEAR OPTIMAL CONTROL TECHNIQUES APPLIED TO A LAUNCH VEHICLE AUTOPILOT. JOURNAL OF AEROSPACE SCIENCE AND TECHNOLOGY (JAST)[Internet]. 2006;3(1):43-49. Available from: https://sid.ir/paper/290935/en

    IEEE: Copy

    M. IRANI RAHAGHI, and J. ROSHANIAN, “NONLINEAR OPTIMAL CONTROL TECHNIQUES APPLIED TO A LAUNCH VEHICLE AUTOPILOT,” JOURNAL OF AEROSPACE SCIENCE AND TECHNOLOGY (JAST), vol. 3, no. 1, pp. 43–49, 2006, [Online]. Available: https://sid.ir/paper/290935/en

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