UPTO NoW HAVE CONJSI DERED PROBLEMS RELEVANT To THE RIGID BO0Y OYNAMICS THAT ARE IMPORTANT To AEROSPACE VEHICLES USED A BODy FRAME THAT ROTATES WITH THE VEHICLE ANOTHER TMPORTANT CLASS oF PRoBLEMS FoR Bo DIES SUCH AS GyRoscofes ROToR WITH HIGH SPIN RATE ESSENTIALY MASSLESS FRAME

Aircraft Lateral Dynamics Using a procedure similar to the longitudinal case, we can develop the equa tions of motion for the lateral dynamics

Longitudinal equations (1-15) can be rewritten as: mu Xuu+ Xww-mg cos 0+ m(w-qUo) =Zuu+ Zww+ Zq-mg sin 000+Z Iyyg =Muu+ Mww+ Mw++ There is no roll/yaw motion, so q 0

ecturt (SpaceCraf AHiud Dynamnics Gal:《GecuwAskwJwy《九 physicald woumics a Hi tude wotiar of spncecraft Ttroduce/ affitude confrol Spaceca+: Pos:tion Linear Vilocity Orb: Motiou Fray! Fuafas motion goverx

一、血流动力学改变 1.左PDA右分流肺循环体循环 2.心脏负荷左房、左室↑右室 3.肺动脉高压

先天性心脏病 一、血液动力学与症状体征 左向右分流 肺循环充血:呼吸道感染

西安电子科技大学：《神经网络与模糊系统 Neural Networks and Fuzzy Systems》课程PPT课件讲稿（2003）04. 突触动力学Ⅱ：有监督学习 Synaptic Dynamics II——Supervised Learning（2/2）

西安电子科技大学：《神经网络与模糊系统 Neural Networks and Fuzzy Systems》课程PPT课件讲稿（2003）04. 突触动力学Ⅱ：有监督学习 Synaptic Dynamics II——Supervised Learning（1/2）

河南大学：《药理学》课程教学资源（讲义）附录——某些药物代谢动力学数据

一、可压缩流动的基本特征: x The pivotal aspect of high -speed flow is that the density is avariable一一密度是变量