Hybrid Intelligent Predictive Control System for High Speed BLDC Motor in Aerospace Application

This paper introduces a design and implementation of Hybrid approaches to control a wings valve using BLDC motor for a Aircraft. The control architecture consists of two layers of control, namely the opening and close speed associated control and the torque assist control. This has been realized by torque sensor and sensor interfaced in the DSP. A disturbance observer (DOB) based controller using the derived dynamic models is also proposed for robust hovering control. The control input induced by DOB is helpful to use simple equations of motion satisfying accurately derived dynamics. For implementing in the system, a DSP-based BLDC motor controller with three-phase inverter module (TMS 320F2812) is used.