文章根据载货汽车的特点对其模型进行了简化,建立了十一自由度的多刚体系统动力学模型;以卡尔丹角描述载货汽车多刚体系统的姿态,运用多刚体系统动力学建模方法,建立了载货汽车十一自由度平顺性动力学模型及其动力学方程;激励分析中考...文章根据载货汽车的特点对其模型进行了简化,建立了十一自由度的多刚体系统动力学模型;以卡尔丹角描述载货汽车多刚体系统的姿态,运用多刚体系统动力学建模方法,建立了载货汽车十一自由度平顺性动力学模型及其动力学方程;激励分析中考虑了轮胎径向跳动的影响,采用逆快速傅里叶变换(inverse fast Fourier transform,IFFT)法建立了四轮相关路面随机输入时域模型;在此基础上,利用Matlab的GUI模块开发了载货汽车平顺性时域仿真系统,并以某型号载货汽车为例进行了平顺性时域仿真;最后,通过载货汽车平顺性实验,验证了该系统的仿真结果是准确可靠的。该系统实现了载货汽车多刚体系统的参数化建模与仿真,能有效地对载货汽车平顺性进行性能预测和评估。展开更多
This article investigates the dynamic characteristics of deflectable nose missiles with rotary single-channel control. After introduction of effective attack and sideslip angles as well as quasi-body coordinates based...This article investigates the dynamic characteristics of deflectable nose missiles with rotary single-channel control. After introduction of effective attack and sideslip angles as well as quasi-body coordinates based on the spin characteristics of the missile＇s body, an integrated rigid kinetic model of missile with deflectable nose control is set up in the quasi-body coordinates considering the interaction between the missile＇s nose and body by using rootless multi-rigid-body system dynamics and is linearized. Then an analysis with simulation is conducted to investigate the coupling characteristics between the channels, the influences of nose deflection on the body and the dynamic characteristics of missile＇s body. The results indicate that various channels of missiles with deflectable nose control are coupled cross-linked; the nose deflection tends to make the body move in the opposite direction and, finally, evidences the correctness and reasonability of the kinetic model proposed by this article.展开更多
文摘文章根据载货汽车的特点对其模型进行了简化,建立了十一自由度的多刚体系统动力学模型;以卡尔丹角描述载货汽车多刚体系统的姿态,运用多刚体系统动力学建模方法,建立了载货汽车十一自由度平顺性动力学模型及其动力学方程;激励分析中考虑了轮胎径向跳动的影响,采用逆快速傅里叶变换(inverse fast Fourier transform,IFFT)法建立了四轮相关路面随机输入时域模型;在此基础上,利用Matlab的GUI模块开发了载货汽车平顺性时域仿真系统,并以某型号载货汽车为例进行了平顺性时域仿真;最后,通过载货汽车平顺性实验,验证了该系统的仿真结果是准确可靠的。该系统实现了载货汽车多刚体系统的参数化建模与仿真,能有效地对载货汽车平顺性进行性能预测和评估。
基金Weapons Preliminary Research Key Foundation of China (9140A01010106HK0307)
文摘This article investigates the dynamic characteristics of deflectable nose missiles with rotary single-channel control. After introduction of effective attack and sideslip angles as well as quasi-body coordinates based on the spin characteristics of the missile＇s body, an integrated rigid kinetic model of missile with deflectable nose control is set up in the quasi-body coordinates considering the interaction between the missile＇s nose and body by using rootless multi-rigid-body system dynamics and is linearized. Then an analysis with simulation is conducted to investigate the coupling characteristics between the channels, the influences of nose deflection on the body and the dynamic characteristics of missile＇s body. The results indicate that various channels of missiles with deflectable nose control are coupled cross-linked; the nose deflection tends to make the body move in the opposite direction and, finally, evidences the correctness and reasonability of the kinetic model proposed by this article.
