A Nonlinear Method of Designing Control System Applied to BTT UAV
Xiaoping Zhu
Abstract
Xiaoping Zhu
Abstract
In this paper,a method of designing control system applied to BTT UAV based on dynamic inversion and variable structure control is proposed.Firstly,the control system of UAV is divided into two subsystem based on time scale method.Then,in very subsystem,the control law is designed based on dynamic inversion and variable structure control theory,the robust of control system is improved because of the application of variable structure control.Finally,the numerical simulation has proved that the method of designing control system applied to BTT UAV based on dynamic inversion and variable structure control is effective.
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In this paper,a method of designing control system applied to BTT UAV based on dynamic inversion and variable structure control is proposed.Firstly,the control system of UAV is divided into two subsystem based on time scale method.Then,in very subsystem,the control law is designed based on dynamic inversion and variable structure control theory,the robust of control system is improved because of the application of variable structure control.Finally,the numerical simulation has proved that the method of designing control system applied to BTT UAV based on dynamic inversion and variable structure control is effective.
Key concepts: Variable structure control, Inversion (geology), Control theory (sociology), Nonlinear system, Computer science, Variable (mathematics), Control system, Control engineering