Based on the flow characteristic equation of air in adiabatic process, the characteristics of modulated on-off valve in a pneumatic pressure control system is analyzed theoretically. The relationship between the param...Based on the flow characteristic equation of air in adiabatic process, the characteristics of modulated on-off valve in a pneumatic pressure control system is analyzed theoretically. The relationship between the parameters and performance of the system is obtained, and it is also observed that the control error is proportional to the on-off period of the valve.展开更多
The aircraft antiskid braking system is an important hydraulic system for preventing tire bursts and ensuring safe take-off and landing. The brake system adjusts the force applied on the brake discs by controlling the...The aircraft antiskid braking system is an important hydraulic system for preventing tire bursts and ensuring safe take-off and landing. The brake system adjusts the force applied on the brake discs by controlling the brake pressure. Traditional aircraft antiskid braking systems achieve antiskid performance by controlling the braking pressure with an electrohydraulic servo valve.Because the pilot stage of an electrohydraulic servo valve is easily blocked by carbonized hydraulic oil, the servo valve would become a dangerous weak point for aircraft safety. This paper proposes a new approach that uses an on-off valve array to replace the servo valve for pressure control. Based on this new pressure control component, an efficient antiskid control algorithm that can utilize this discontinuous feature is proposed. Furthermore, the algorithm has the ability to identify the runway circumstances. To overcome the discontinuity in the process of using an on-off valve array, the Filippov framework is introduced. The conditions of convergence of the system are also discussed.The results of the digital simulations and the hardware-in-the-loop(HIL) braking experiments are used to verify the efficiency and stability of the proposed control algorithm. The method also proves that the on-off valve array can replace the servo valve perfectly as a new type of antiskid braking pressure control component.展开更多
文摘Based on the flow characteristic equation of air in adiabatic process, the characteristics of modulated on-off valve in a pneumatic pressure control system is analyzed theoretically. The relationship between the parameters and performance of the system is obtained, and it is also observed that the control error is proportional to the on-off period of the valve.
基金the Science and Technology on Aircraft Control Laboratorythe National Nature Science Foundation of China (Nos. 51775014 and 51890882)
文摘The aircraft antiskid braking system is an important hydraulic system for preventing tire bursts and ensuring safe take-off and landing. The brake system adjusts the force applied on the brake discs by controlling the brake pressure. Traditional aircraft antiskid braking systems achieve antiskid performance by controlling the braking pressure with an electrohydraulic servo valve.Because the pilot stage of an electrohydraulic servo valve is easily blocked by carbonized hydraulic oil, the servo valve would become a dangerous weak point for aircraft safety. This paper proposes a new approach that uses an on-off valve array to replace the servo valve for pressure control. Based on this new pressure control component, an efficient antiskid control algorithm that can utilize this discontinuous feature is proposed. Furthermore, the algorithm has the ability to identify the runway circumstances. To overcome the discontinuity in the process of using an on-off valve array, the Filippov framework is introduced. The conditions of convergence of the system are also discussed.The results of the digital simulations and the hardware-in-the-loop(HIL) braking experiments are used to verify the efficiency and stability of the proposed control algorithm. The method also proves that the on-off valve array can replace the servo valve perfectly as a new type of antiskid braking pressure control component.
基金This research was financially supported by National Natural Science Foundation of China(51705445),Natural Science Foundation of Hebei Province of China(E2016203324),Open Foundation of the State Key Laboratory of Fluid Power and Mechatronic Systems(GZKF-20
