When the aircraft tow tractor encounters slippery, icy, oily, or debris-covered ground, as well as situations such as overloaded towing, uneven aircraft weight distribution, sharp acceleration and turns, brake system malfunctions, or severely worn tires, it may slip due to a mismatch between traction force and ground adhesion. The slipping of aircraft tug is prone to cause the aircraft to lose control and collide, resulting in damage, flight delays or cancellations, posing a major safety hazard and affecting the smooth operation of the airport. Brake control is crucial to the safety of aircraft tow tractors. The Anti-lock Braking System (ABS) prevents wheel lock-up in aircraft tow tractors, ensuring vehicle stability during braking and avoiding loss of control. The Traction Control System (TCS) optimizes traction, prevents wheel slip, and enhances stability during starting, accelerating, and turning. Together, they improve the safety and handling of aircraft tow tractors under complex ground conditions. This study establishes a traction control scheme that combines TCS operation with electromagnetic braking to prevent wheel slip during starting, accelerating, or turning of aircraft tow tractors. Additionally, a novel tracking control design is proposed for aircraft tow tractors, integrating driving and braking functions into a single module. When the motor rotates, it generates back-electromotive force (back-EMF), which is utilized to produce braking force. By adjusting the switching sequence of the inverter and the duty cycle of Pulse Width Modulation (PWM), the magnetic fields of the front and rear motors are controlled to generate appropriate braking torque for rapid braking. This design has been verified through actual testing. It prevents the vehicle from slipping during driving and effectively enhances braking performance.