The current research of air suspension mainly focuses on the characteristics and design of the air spring. In fact, electronically controlled air suspension （ECAS） has excellent performance in flexible height adjust...The current research of air suspension mainly focuses on the characteristics and design of the air spring. In fact, electronically controlled air suspension （ECAS） has excellent performance in flexible height adjustment during different driving conditions. However, the nonlinearity of the ride height adjusting system and the uneven distribution of payload affect the control accuracy of ride height and the body attitude. Firstly, the three-point measurement system of three height sensors is used to establish the mathematical model of the ride height adjusting system. The decentralized control of ride height and the centralized control of body attitude are presented to design the ride height control system for ECAS. The exact feedback linearization method is adopted for the nonlinear mathematical model of the ride height system. Secondly, according to the hierarchical control theory, the variable structure control （VSC） technique is used to design a controller that is able to adjust the ride height for the quarter-vehicle anywhere, and each quarter-vehicle height control system is independent. Meanwhile, the three-point height signals obtained by three height sensors are tracked to calculate the body pitch and roll attitude over time, and then by calculating the deviation of pitch and roll and its rates, the height control correction is reassigned based on the fuzzy algorithm. Finally, to verify the effectiveness and performance of the proposed combined control strategy, a validating test of ride height control system with and without road disturbance is carried out. Testing results show that the height adjusting time of both lifting and lowering is over 5 s, and the pitch angle and the roll angle of body attitude are less than 0.15°. This research proposes a hierarchical control method that can guarantee the attitude stability, as well as satisfy the ride height tracking system.展开更多
电控空气悬架(electronically controlled air suspension,ECAS)系统的有效控制依赖于传感器实时采集的正确车身状态信号。针对电控空气悬架传感器卡死、恒偏差、恒增益3种故障,建立1种ECAS故障检测与隔离方法(fault detection and isol...电控空气悬架(electronically controlled air suspension,ECAS)系统的有效控制依赖于传感器实时采集的正确车身状态信号。针对电控空气悬架传感器卡死、恒偏差、恒增益3种故障,建立1种ECAS故障检测与隔离方法(fault detection and isolation,FDI)。建立电控空气悬架三自由度1/4车模型以及传感器故障时空气悬架模型,设计故障检测滤波器组,结合传感器实时测量值获得空气悬架输出残差,在此基础上确定故障检测指标,计算指标数值并选取适当阈值进行比较。诊断滤波器采用强跟踪滤波器方法进行设计,选取两级决策变量构造隔离决策函数,实现对故障传感器的检测与隔离。仿真分析表明,所提出的基于STF的方法实现了ECAS传感器故障的检测与隔离,有效提高了车辆控制的可靠性与安全性。展开更多
为解决电控空气悬架(electric control air suspension,简称ECAS)车身高度切换过程中的振荡及"过充"、"过放"现象,以空气弹簧特性为媒介,与车辆动力学相结合,对车身高度调节系统的进行建模。通过遗传算法优化车身...为解决电控空气悬架(electric control air suspension,简称ECAS)车身高度切换过程中的振荡及"过充"、"过放"现象,以空气弹簧特性为媒介,与车辆动力学相结合,对车身高度调节系统的进行建模。通过遗传算法优化车身高度调节系统PID的控制参数,提出一种新的积分分离PID控制策略。采用Matlab/Simulink搭建模型并对控制前、后仿真结果进行了对比。结果证明,所设计的控制方法能有效解决以上问题,优化后的车身高度调节系统能显著减少汽车振荡及干扰,操纵稳定性得到改善。展开更多
提出电控空气悬架(Electronically Controlled Air Suspension,ECAS)的参数自整定模糊PID控制策略,设计参数自整定模糊PID控制器。利用AMESim软件建立1/4电控空气悬架系统模型,采用Matlab/Simulink和AMESim在不同路面、不同车速下对空...提出电控空气悬架(Electronically Controlled Air Suspension,ECAS)的参数自整定模糊PID控制策略,设计参数自整定模糊PID控制器。利用AMESim软件建立1/4电控空气悬架系统模型,采用Matlab/Simulink和AMESim在不同路面、不同车速下对空气悬架系统分别进行PID控制与参数自整定模糊PID控制策略下的联合仿真。仿真结果表明:与PID控制仿真比较,采用参数自整定模糊PID控制策略使电控空气悬架的性能指标得到显著改善。搭建1/4电控空气悬架试验台,利用电液伺服激振台进行激励加载,完成硬件在环实时仿真测试,试验结果证明采用参数自整定模糊PID控制能有效提高悬架的总体性能。展开更多
基金Supported by National Natural Science Foundation of China(Grant No.51105177)Jiangsu Provincial Natural Science Foundation of China(Grant No.BK20131255)+2 种基金Research Fund for the Doctoral Program of Higher Education of China(Grant No.20113227120015)Qing Lan Project of Jiangsu Province of China,Scientific Research Foundation for Advanced Talents,Jiangsu University,China(Grant No.11JDG047)Hunan Provincial Natural Science Foundation of China(Grant No.12JJ6036)
文摘The current research of air suspension mainly focuses on the characteristics and design of the air spring. In fact, electronically controlled air suspension （ECAS） has excellent performance in flexible height adjustment during different driving conditions. However, the nonlinearity of the ride height adjusting system and the uneven distribution of payload affect the control accuracy of ride height and the body attitude. Firstly, the three-point measurement system of three height sensors is used to establish the mathematical model of the ride height adjusting system. The decentralized control of ride height and the centralized control of body attitude are presented to design the ride height control system for ECAS. The exact feedback linearization method is adopted for the nonlinear mathematical model of the ride height system. Secondly, according to the hierarchical control theory, the variable structure control （VSC） technique is used to design a controller that is able to adjust the ride height for the quarter-vehicle anywhere, and each quarter-vehicle height control system is independent. Meanwhile, the three-point height signals obtained by three height sensors are tracked to calculate the body pitch and roll attitude over time, and then by calculating the deviation of pitch and roll and its rates, the height control correction is reassigned based on the fuzzy algorithm. Finally, to verify the effectiveness and performance of the proposed combined control strategy, a validating test of ride height control system with and without road disturbance is carried out. Testing results show that the height adjusting time of both lifting and lowering is over 5 s, and the pitch angle and the roll angle of body attitude are less than 0.15°. This research proposes a hierarchical control method that can guarantee the attitude stability, as well as satisfy the ride height tracking system.
文摘电控空气悬架(electronically controlled air suspension,ECAS)系统的有效控制依赖于传感器实时采集的正确车身状态信号。针对电控空气悬架传感器卡死、恒偏差、恒增益3种故障,建立1种ECAS故障检测与隔离方法(fault detection and isolation,FDI)。建立电控空气悬架三自由度1/4车模型以及传感器故障时空气悬架模型,设计故障检测滤波器组,结合传感器实时测量值获得空气悬架输出残差,在此基础上确定故障检测指标,计算指标数值并选取适当阈值进行比较。诊断滤波器采用强跟踪滤波器方法进行设计,选取两级决策变量构造隔离决策函数,实现对故障传感器的检测与隔离。仿真分析表明,所提出的基于STF的方法实现了ECAS传感器故障的检测与隔离,有效提高了车辆控制的可靠性与安全性。
文摘为解决电控空气悬架(electric control air suspension,简称ECAS)车身高度切换过程中的振荡及"过充"、"过放"现象,以空气弹簧特性为媒介,与车辆动力学相结合,对车身高度调节系统的进行建模。通过遗传算法优化车身高度调节系统PID的控制参数,提出一种新的积分分离PID控制策略。采用Matlab/Simulink搭建模型并对控制前、后仿真结果进行了对比。结果证明,所设计的控制方法能有效解决以上问题,优化后的车身高度调节系统能显著减少汽车振荡及干扰,操纵稳定性得到改善。
文摘提出电控空气悬架(Electronically Controlled Air Suspension,ECAS)的参数自整定模糊PID控制策略,设计参数自整定模糊PID控制器。利用AMESim软件建立1/4电控空气悬架系统模型,采用Matlab/Simulink和AMESim在不同路面、不同车速下对空气悬架系统分别进行PID控制与参数自整定模糊PID控制策略下的联合仿真。仿真结果表明:与PID控制仿真比较,采用参数自整定模糊PID控制策略使电控空气悬架的性能指标得到显著改善。搭建1/4电控空气悬架试验台,利用电液伺服激振台进行激励加载,完成硬件在环实时仿真测试,试验结果证明采用参数自整定模糊PID控制能有效提高悬架的总体性能。
