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Information Journal Paper

Title

GUIDANCE LAW DESIGN USING FINITE TIME SECOND ORDER SLIDING MODE CONTROL

Pages

  36-44

Abstract

 In this paper, a two point GUIDANCE LAW for homing interceptors using finite time SECOND ORDER SLIDING MODE control and based on PARALLEL NAVIGATION is proposed. In the proposed GUIDANCE LAW, sliding surface is selected as the line of sight rate and the target maneuvers are considered as an uncertainty which only needs the upper bound of these maneuvers. Furthermore, the proposed algorithm can guarantee the finite time convergence of the LOS rate to zero or a small neighborhood of zero. Therefore, the performance and stability of guidance loop against maneuvering targets are increased.

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    APA: Copy

    BEHNAM GOL, VAHID, MOHAMMADZAMAN, IMAN, VALI, AHMAD REZA, & GHAHRAMANI, NEMAT OLLAH. (2011). GUIDANCE LAW DESIGN USING FINITE TIME SECOND ORDER SLIDING MODE CONTROL. JOURNAL OF CONTROL, 5(3), 36-44. SID. https://sid.ir/paper/120793/en

    Vancouver: Copy

    BEHNAM GOL VAHID, MOHAMMADZAMAN IMAN, VALI AHMAD REZA, GHAHRAMANI NEMAT OLLAH. GUIDANCE LAW DESIGN USING FINITE TIME SECOND ORDER SLIDING MODE CONTROL. JOURNAL OF CONTROL[Internet]. 2011;5(3):36-44. Available from: https://sid.ir/paper/120793/en

    IEEE: Copy

    VAHID BEHNAM GOL, IMAN MOHAMMADZAMAN, AHMAD REZA VALI, and NEMAT OLLAH GHAHRAMANI, “GUIDANCE LAW DESIGN USING FINITE TIME SECOND ORDER SLIDING MODE CONTROL,” JOURNAL OF CONTROL, vol. 5, no. 3, pp. 36–44, 2011, [Online]. Available: https://sid.ir/paper/120793/en

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