Linear Scheduled Controller for Nonlinear UAV Pitch Plane Operations
نویسندگان
چکیده
The nonlinear air vehicles can be linearized about desired equilibrium points and a linear controller can be designed which stabilizes the aircraft about that equilibrium point. A mission planning is considered as taking the nonlinear system through different equilibrium points. Thus there will be different linear systems for each equilibrium point. To design a controller that drives the system through different equilibrium points, gain scheduling technique is used. Enough equilibrium points are used to keep equilibrium points intact. Keywords— Autonomous UAV, Nonlinear systems, switching equilibrium, Stability Embedded Control.
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تاریخ انتشار 2014