“…Assuming that the pressure gap between two portals of tunnels is zero, and traffic intensity remains stable in one control period, we can first use the original tunnel aerodynamic (2) to serve as the base for our system model [2,18,22,23]. We then re-write (2) into (3) in order to model the relationship between system input v j , disturbances v + , v − , K + , K − and state u (see (2) and 3)where N j is the number of jet fans inside the tunnel, A f is the section area of jet fan (m 2 ), k j is the pressure rise coefficient of fans, L is the tunnel length (m), c d is the average drag coefficient of the vehicle platoon and A v,m is the equivalent vehicle windward area (m 2 ), which is the weighted average of products of the windward area and the drag coefficient of all the vehicle types.…”