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Command filtered integrated estimation guidance and control for strapdown missiles with circular field of view
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In this paper,an integrated estimation guidance and control(IEGC)system is designed based on the command filtered backstepping approach for circular field-of-view(FOV)strapdown missiles.The three-dimensional integrated estimation guidance and control nonlinear model with limited actuator deflec-tion angle is established considering the seeker's FOV constraint.The boundary time-varying integral barrier Lyapunov function(IBLF)is employed in backstepping design to constrain the body line-of-sight(BLOS)in IEGC system to fit a circular FOV.Then,the nonlinear adaptive controller is designed to esti-mate the changing aerodynamic parameters.The generalized extended state observer(GESO)is designed to estimate the acceleration of the maneuvering targets and the unmatched time-varying disturbances for improving tracking accuracy.Furthermore,the command filters are used to solve the"differential expansion"problem during the backstepping design.The Lyapunov theory is used to prove the stability of the overall closed-loop IEGC system.Finally,the simulation results validate the integrated system's effectiveness,achieving high accuracy strikes against maneuvering targets.
Integrated estimation guidance and controlCircular field-of-viewTime-varying integral barrier Lyapunov functionCommand filtered backstepping controlNonlinear adaptive controlExtended state observer
Wei Wang、Jiaqi Liu、Shiyao Lin、Baokui Geng、Zhongjiao Shi
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School of Aerospace Engineering,Beijing Institute of Technology,Beijing 10081,China
China Research and Development Academy of Machinery Equipment,Beijing 100089,China
Northwest Industries Group CO.,Ltd.,Xi'an 710043,China
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