A NOVEL OPTIMAL ROBUST GUIDANCE LAW DESIGN BASED ON EXTENDED KALMAN FILTER

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MOOSAPOUR S.H.; MOOSAPOUR S.S.

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Paper Information

Journal: Journal of Aerospace Mechanics Year:2016 | Volume:11 | Issue:4 (42) (DYNAMICS, VIBRATIONS AND CONTROL) Page(s): 39-48

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Information Journal Paper

Title

A NOVEL OPTIMAL ROBUST GUIDANCE LAW DESIGN BASED ON EXTENDED KALMAN FILTER

Author(s)

MOOSAPOUR S.H. | MOOSAPOUR S.S. | Issue Writer Certificate

Keywords

SLIDING MODE CONTROLQ1

BACKSTEPPING APPROACHQ2

GENETIC ALGORITHMQ2

GUIDANCEQ2

AUGMENTED PROPORTIONAL NAVIGATIONQ2

Abstract

In this paper a novel optimal and robust GUIDANCE law for three dimensional flying-object system is proposed based on the extended kalman filter. New GUIDANCE law consists of sliding mode and backstepping GUIDANCE laws. In this GUIDANCE law there are some coefficients that must be adjusted. These coefficients are adjusted using GENETIC ALGORITHM (GA). Also system states are estimated by using of Continues Extended Kalman Filter (CEKF). Finally, proposed GUIDANCE law is compared with AUGMENTED PROPORTIONAL NAVIGATION GUIDANCE (APNG) law. Simulation results show that proposed GUIDANCE law is better than APNG law.

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APA: Copy

MOOSAPOUR, S.H., & MOOSAPOUR, S.S.. (2016). A NOVEL OPTIMAL ROBUST GUIDANCE LAW DESIGN BASED ON EXTENDED KALMAN FILTER. AEROSPACE MECHANICS JOURNAL, 11(4 (42) (DYNAMICS, VIBRATIONS AND CONTROL)), 39-48. SID. https://sid.ir/paper/101995/en

Vancouver: Copy

MOOSAPOUR S.H., MOOSAPOUR S.S.. A NOVEL OPTIMAL ROBUST GUIDANCE LAW DESIGN BASED ON EXTENDED KALMAN FILTER. AEROSPACE MECHANICS JOURNAL[Internet]. 2016;11(4 (42) (DYNAMICS, VIBRATIONS AND CONTROL)):39-48. Available from: https://sid.ir/paper/101995/en

IEEE: Copy

S.H. MOOSAPOUR, and S.S. MOOSAPOUR, “A NOVEL OPTIMAL ROBUST GUIDANCE LAW DESIGN BASED ON EXTENDED KALMAN FILTER,” AEROSPACE MECHANICS JOURNAL, vol. 11, no. 4 (42) (DYNAMICS, VIBRATIONS AND CONTROL), pp. 39–48, 2016, [Online]. Available: https://sid.ir/paper/101995/en

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