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Information Journal Paper

Title

A NOVEL ROBUST PROPORTIONAL NAVIGATION GUIDANCE LAW FOR SURFACE-TO-AIR MISSILE BASED ON EXTENDED KALMAN FILTER

Pages

  33-48

Abstract

 In this paper a novel optimal and robust PROPORTIONAL NAVIGATION (PN) GUIDANCE law for three dimensional MISSILE-target system is proposed based on extended Kalman filter (EKF). New GUIDANCE law is a combination of PN, sliding mode and BACK STEPPING GUIDANCE laws. In this GUIDANCE law there are some coefficients that must be adjusted. GENETIC algorithm (GA) is used to achieve this goal. Also, system states are estimated using extended Kalman-Bucy filter (EKBF). Finally, proposed GUIDANCE law (PN BACK STEPPING (PNB)) is compared with augmented PROPORTIONAL NAVIGATION GUIDANCE (APNG) law. Simulation results indicate that PNB law has far better performance compared to APNG law.

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  • Cite

    APA: Copy

    MOOSAPOUR, SEYED HAMZE, & EDRISI, MAHDI. (2014). A NOVEL ROBUST PROPORTIONAL NAVIGATION GUIDANCE LAW FOR SURFACE-TO-AIR MISSILE BASED ON EXTENDED KALMAN FILTER. JOURNAL OF AERONAUTICAL ENGINEERING (JOAE), 16(1), 33-48. SID. https://sid.ir/paper/173119/en

    Vancouver: Copy

    MOOSAPOUR SEYED HAMZE, EDRISI MAHDI. A NOVEL ROBUST PROPORTIONAL NAVIGATION GUIDANCE LAW FOR SURFACE-TO-AIR MISSILE BASED ON EXTENDED KALMAN FILTER. JOURNAL OF AERONAUTICAL ENGINEERING (JOAE)[Internet]. 2014;16(1):33-48. Available from: https://sid.ir/paper/173119/en

    IEEE: Copy

    SEYED HAMZE MOOSAPOUR, and MAHDI EDRISI, “A NOVEL ROBUST PROPORTIONAL NAVIGATION GUIDANCE LAW FOR SURFACE-TO-AIR MISSILE BASED ON EXTENDED KALMAN FILTER,” JOURNAL OF AERONAUTICAL ENGINEERING (JOAE), vol. 16, no. 1, pp. 33–48, 2014, [Online]. Available: https://sid.ir/paper/173119/en

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