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Matthew C. Best 《Vehicle System Dynamics: International Journal of Vehicle Mechanics and Mobility》2019,57(1):64-85
In recent years the application of driver steering models has extended from the off-line simulation environment to autonomous vehicles research and the support of driver assistance systems. For these new environments there is a need for the model to be adaptive in real time, so the supporting vehicle systems can react to changes in the driver, their driving style, mood and skill. This paper provides a novel means to meet these needs by combining a simple driver model with a single-track vehicle handling model in a parameter estimating filter – in this case, an unscented Kalman filter. Although the steering model is simple, a motion simulator study shows it is capable of characterising a range of driving styles and may also indicate the level of skill of the driver. The resulting filter is also efficient – comfortably operating faster than real time – and it requires only steer and speed measurements from the vehicle in addition to the reference path. Adaptation of the steer model parameters is demonstrated along with robustness of the filter to errors in initial conditions, using data from five test drivers in vehicle tests carried out on the open road.
Abbreviations: ADAS: advanced driver assistance systems; CG: centre of gravity; CAN: controller area network; EKF: extended Kalman filter; GPS: global positioning system; UKF: unscented Kalman filter 相似文献
503.
对无砟轨道吸声板降噪措施效果的评价与分析 总被引:1,自引:0,他引:1
马筠 《铁道劳动安全卫生与环保》2008,35(3):111-114
对框架型和双块式无砟轨道结构铺设吸声板前后进行了列车辐射噪声测试,结果表明:在距线路中心线3.75m、于轨面1.5m处,框架型板式无砟轨道结构噪声降低约2dB(A),双块式无砟轨道结构降低约1dB(A),该吸声板的吸声系数在315~3150Hz的中高频段有较好的吸声效果,能够有效吸收列车通过时主要分布在500~4000Hz中高频段的辐射噪声能量,具有一定的吸声效果。并对产生不同吸声效果的原因进行了分析。该测试结果可供铁路建设项目环境影响评价参考和借鉴。 相似文献
504.
A novel joint source channel distortion model was proposed, which can essentially estimate the average distortion in progressive image transmission. To improve the precision of the model, the redundancy generated by a forbidden symbol in the arithmetic codes is used to distinguish the quantization distortion and the channel distortion, all the coefficients from the first error one to the end of the sequence are set to be a value within the variance range of the coefficients instead of zero, then the error propagation coming from the entropy coding can be essentially estimated, which is disregarded in the most conventional joint source channel coding (JSCC) systems. The precision of the model in terms of average peak-signal-to-noise has been improved about 0.5 dB compared to classical works. An efficient unequal error protection system based on the model is developed, and can be used in the wireless communication systems. 相似文献
505.
本文根据新校区校园网的规划和建设历程,探讨了针对当前新校区校园网建设所涉及的具体规划原则和方法,提出了现阶段新校区网络技术的选择标准。 相似文献
506.
重点研究了一种基于灵敏度矩阵对桥梁进行损伤识别的方法。基于振动分析的矩阵摄动理论,首先讨论了求取模态参数对结构物理参数灵敏度矩阵的方法,形成灵敏度矩阵的过程中避免了偏微分计算;基于灵敏度矩阵,建立了桥梁的损伤识别模型,并给出了此模型具体的求解方法;然后利用Guyan缩减的方法来缩减结构的模态自由度,保证了在进行损伤识别的过程中利用较少的模态参数,进而提高了方法的实用性;最后把所述方法应用于三跨预应力混凝土连续箱梁桥的实际损伤诊断工程。结果表明,利用所述方法进行预应力混凝土连续梁桥的损伤识别是有效的。 相似文献
507.
Aircraft icing accident happens frequently. Researchers try to find new ways to solve this problem. The study is facing the direction of intelligent inspection and control system. Previous studies focused on the principle of aircraft icing and its effects on flight performance. The onboard icing detection equipment can only give the qualitative icing information, but cannot effectively describe how serious the consequences would be. If the icing detection equipment fails, it will cause a serious threat to flight safety. This paper reviews the smart icing system and its fundamental principle. Then based on H∞ theory, an aircraft icing parameter identification method is introduced, and its feasibility is verified by simulation results. Moreover, this method can work normally under noise interference and measurement error. Icing parameter identification method can also test part of aircraft’s stability or control derivatives which would be changed obviously after aircraft icing. Classified by neural networks, the stability or control derivatives’ variation can be mapped to ice parameters’ variation that reflects the severity of aircraft icing. Then H2 state feedback control is designed originally to suppress the impact of noise interference, so aircraft can keep steady after it is iced. Seeing from simulation result of the whole system, it is clear that the system can effectively detect icing parameters and by using feedback control system, it can ensure the safety of aircraft in the flight envelope. 相似文献
508.
机场刚性道面地基参数识别研究 总被引:2,自引:0,他引:2
提出一种机场刚性道面无损检测中的地基反应模量K的动态识别方法,以运动荷载作用下的粘弹性Winkler地基上的板系统的动态力学计算模型的方程解析解为基础,应用最小二乘方准则来拟合实测动挠度和理论动挠度,从而识别出地基反应模量K。通过实例计算,表明识别结果可靠。 相似文献
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