Title: Second Order Nonsingular Terminal Sliding Mode Guidance Law for Intercepting with Desired Impact Angle

سال انتشار: 1394
نوع سند: مقاله کنفرانسی
زبان: انگلیسی
مشاهده: 634

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شناسه ملی سند علمی:

MAARS01_140

تاریخ نمایه سازی: 16 اسفند 1394

چکیده مقاله:

Second order non-singular terminal sliding mode guidance for intercepting with desired impact angle in terminal phase is proposed in this paper. In order to satisfy the predefined impact angle and interception into target, a non-singular terminal sliding variable is introduced using line of sight angle error and line of sight angular rate. In reaching phase in the presence of uncertainties such as target maneuvers, second order sliding mode guidance law and sliding mode observer is designed in order to zeroing the sliding variable. Then in sliding phase, due to introducing non-singular terminal sliding variable, finite time stability of line of sight angle and line of sight angular rate is grantee without singularity in commanded acceleration as control signal. Numerical simulations are presented to illustrate the potential of the proposed guidance law.

نویسندگان

Reza Fattahian

MSc Student, Islamic Azad University Damavand Branch, Damavand.

Ahmadreza Vali

Assosiate Professor, Islamic Azad University Damavand Branch, Damavand,

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