A Study on Brake Control Strategy for the UAV All-Electric Brake System

Aiming at the emergency braking and rapid response of the Unmanned Aerial Vehicle (UAV) operating on the ground, a novel brake control strategy is proposed in this paper, adopting an integrated design of pressure and velocity based on sliding mode control. The strategy takes the air travel in the operation of the all-electric brake system into consideration. In this paper, the controller of an UAV Hardware-in-the-Loop (HIL) test system will be used to verify the feasibility of the novel brake control strategy and the simulation results are adopted to validate the superiority and feasibility of the brake control strategy for UAV all-electric brake system.