UAV Anti-Skid Braking System Simulation

A dynamics model of UAV braking is established for simulation, and by analyzing the anti-skid braking system, a dual channel anti -skid braking system based on slip-ratio is presented. The fuzzy control theory is used in the control system, and a balance control system is added between the left wheel and right wheel of UAV. The HIL (hardware in loop) experiment results demonstrate that in different conditions, the anti-skid braking system can automatically regulate the brake pressure and keep the UAV from yawing dramatically.