Design of Control Systems for a Quadrotor Flight Vehicle Equipped With Inertial Sensors
This thesis reviews the Design of Control Systems for a Quadrotor Flight Vehicle Equipped with Inertial Sensors in detail. The control system is developed in Matlab/Simulink and real time implementation is achieved by using Simulink Real Time Windows Target utility. Linear Quadratic Regulator is designed for the stabilization of the attitude and shown to work in real time. The hardware consists of the data acquisition card, DC motor drivers, sensor set, the DC motors, and the DraganFlyer V Ti structure.