DESIGN OF NONLINEAR OPTIMAL GUIDANCE LAW FOR HIGH MANEUVER TARGETS BASED ON STATE DEPENDENT RICCATI EQUATION

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BABAEI ALIREZA; SETAYANDEH SEYYED MOHAMMAD REZA

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Paper Information

Journal: AEROSPACE KNOWLEDGE AND TECHNOLOGY JOURNAL Year:2017 | Volume:6 | Issue:1 Page(s): 93-107

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Title

DESIGN OF NONLINEAR OPTIMAL GUIDANCE LAW FOR HIGH MANEUVER TARGETS BASED ON STATE DEPENDENT RICCATI EQUATION

Author(s)

BABAEI ALIREZA | SETAYANDEH SEYYED MOHAMMAD REZA | Issue Writer Certificate

Keywords

MISSILEQ3

GUIDANCE LAWQ1

STATE DEPENDENT RICCATI EQUATION METHODQ1

Abstract

In this study, a new GUIDANCE LAW for high maneuver targets is designed by using state dependent Riccati equation. The reason of using this equation is: no need to linearization of equations and simplification of implementation. The aim of this research is presenting a GUIDANCE LAW that compensate the depletion of classic GUIDANCE LAWs for high maneuver targets and in the second, the comparison among proportional navigation law, pure pursuit law and new GUIDANCE LAW. It is worth noting that the criterions of analyzing are: total of incoming acceleration and required time for hitting the target. So these laws have been compared for fixed target, moving target with constant speed and moving target with variable speed and for different initial conditions. Finally a sensitivity analysis has been done for investigation of laws behavior.

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APA: Copy

BABAEI, ALIREZA, & SETAYANDEH, SEYYED MOHAMMAD REZA. (2017). DESIGN OF NONLINEAR OPTIMAL GUIDANCE LAW FOR HIGH MANEUVER TARGETS BASED ON STATE DEPENDENT RICCATI EQUATION. AEROSPACE KNOWLEDGE AND TECHNOLOGY JOURNAL, 6(1 ), 93-107. SID. https://sid.ir/paper/264151/en

Vancouver: Copy

BABAEI ALIREZA, SETAYANDEH SEYYED MOHAMMAD REZA. DESIGN OF NONLINEAR OPTIMAL GUIDANCE LAW FOR HIGH MANEUVER TARGETS BASED ON STATE DEPENDENT RICCATI EQUATION. AEROSPACE KNOWLEDGE AND TECHNOLOGY JOURNAL[Internet]. 2017;6(1 ):93-107. Available from: https://sid.ir/paper/264151/en

IEEE: Copy

ALIREZA BABAEI, and SEYYED MOHAMMAD REZA SETAYANDEH, “DESIGN OF NONLINEAR OPTIMAL GUIDANCE LAW FOR HIGH MANEUVER TARGETS BASED ON STATE DEPENDENT RICCATI EQUATION,” AEROSPACE KNOWLEDGE AND TECHNOLOGY JOURNAL, vol. 6, no. 1 , pp. 93–107, 2017, [Online]. Available: https://sid.ir/paper/264151/en

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