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Cites:

Information Journal Paper

Title

CONTROL DESIGN OF THE SINGLE STAGE SPACE VEHICLE USING EVOLUTIONARY ALGORITHM

Pages

  29-37

Abstract

 A system of flight control should be used by the aerospace launch vehicle (ALV) for reaching to injection point in the orbit. ALV is a dynamic system which is described by mathematical terms which include imprecise dynamic ALV causes controller efficiency to become low, and steady state error is created.Specified cases lead to divergence. In comparison with other control systems, application of the PID controller is the most important advantage of it.Especially PID controllers are useful when there is no specific mathematical model and analytic methods are not utilizable. In this project, using of controller is proposed according to output results of guidance command along the vehicle path. For non-linear system, six degree of freedom ALV equation and considering single stage reaching orbit, also specific initial conditions, and PID controller is designed by the use of GENETIC ALGORITHM.

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    • Cite

    APA: Copy

    NOVIN ZADEH, A.B., PAZOOKI, F., & SARBAZI, M.M.. (2009). CONTROL DESIGN OF THE SINGLE STAGE SPACE VEHICLE USING EVOLUTIONARY ALGORITHM. JOURNAL OF AEROSPACE SCIENCE AND RESEARCH, 2(2), 29-37. SID. https://sid.ir/paper/199479/en

    Vancouver: Copy

    NOVIN ZADEH A.B., PAZOOKI F., SARBAZI M.M.. CONTROL DESIGN OF THE SINGLE STAGE SPACE VEHICLE USING EVOLUTIONARY ALGORITHM. JOURNAL OF AEROSPACE SCIENCE AND RESEARCH[Internet]. 2009;2(2):29-37. Available from: https://sid.ir/paper/199479/en

    IEEE: Copy

    A.B. NOVIN ZADEH, F. PAZOOKI, and M.M. SARBAZI, “CONTROL DESIGN OF THE SINGLE STAGE SPACE VEHICLE USING EVOLUTIONARY ALGORITHM,” JOURNAL OF AEROSPACE SCIENCE AND RESEARCH, vol. 2, no. 2, pp. 29–37, 2009, [Online]. Available: https://sid.ir/paper/199479/en

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