Research on synchronous optimization and anti-skid strategy of aircraft antiskid braking system

In this paper, an aircraft synchronous optimization and synchronous anti-skid control strategy is proposed to reduce the yaw burden during aircraft braking. This study analyses the effect of yaw that may be caused by the friction coefficient of an aircraft during braking. A braking synchronous optimization algorithm is developed that can reduce the skidding phenomenon during the increase pressure process. At the same time, a synchronous anti-skid technology is introduced, which automatically adjusts the braking force by detecting the slip state of the wheels on both sides to reduce the risk of aircraft yawing due to unilateral slip. Through a series of simulations and experiments, it is concluded that the use of synchronous optimization and synchronous anti-skid control strategy can significantly reduce the risk of aircraft running off the runway.