DESIGN AND CONTROL OF SELF-BALANCING COCKPIT FOR SPECIAL COPYRIGHT PLATFORM

The structure design scheme and the control method of a self-balancing cockpit system based on the principle of dual-axis gyro were proposed to solve the problem of improving maneuverability of special copyright platform under large roll and pitch motions.First, the structural modeling of the self-balancing cockpit system was completed by Creo, and

Aiming at improving the torque density of the motor and the utilization rate of permanent magnets (PMs), a dual rotor consequent-pole vernier motor (DRCPVM) is proposed in this article.The stator of the motor has a double-sided structure with two sets of independent windings on each side.Therefore, the proposed motor has different working modes acc