Euler angles are adopted to describe the joint movements.
关节的转动角度采用了欧拉角表述。
The Euler angles could be expressed with arbitrarily large rotations.
这里欧拉角可以用来表示任意大的转动。
This article shows the make and use of the simple Euler Angles model designed by the author herself.
本文介绍了笔者自行设计的简易欧勒角演示模型的制作和使用。
This is due to the fact that Euler angles are always expressed relative to the global coordinate system.
这归咎于欧拉角总是以球坐标系表示。
The teaching practice has showed that it is helpful to use the object in class on the topic of 'Euler Angles "."
教学实践表明：它的使用大有助于“欧勒角”课题的直观教学。
The attitudes of vehicle are described by both quaternion and Euler angles, and two kinds of motion equations are established accordingly.
通过四元数法和欧拉角法描述飞行器姿态，并建立相应的运动学方程。
There are many ways to represent the orientation of an object. Most programmers use 3x3 rotation matrices or three Euler angles to store this information.
有三种办法表示旋转：矩阵表示，欧拉角表示，以及四元组表示。
Compared to the Euler angles the main advantage of the quaternions expression of attitude motion is the avoidance of singular position in numeration procedure.
与欧拉角比较，姿态运动的四元数表达的主要优点是数值计算过程中不存在奇异位置。
The differential equations of equilibrium of the constrained rod are established taking Euler angles as variables to describe the attitude of the cross section.
以描述截面姿态的欧拉角为变量，建立受约束弹性杆的平衡方程。
The evaluation methods and step of the loading for the FMAV are set up so that these Euler angles can be specified to provide wing motions that generate the lift and propulsion for the vehicle.
建立由欧拉角所确定的扑翼飞行器的载荷计算方法和步骤，揭示出扑翼飞行器通过扑翼运动同时产生升力、推力的机理。
The mathematical model is composed of the following parts:1) Basic algorithm library: it covers the definition of coordinate system and Euler angles, as well as simulation algorithm library, etc.
基础算法库：包括常用坐标系定义、欧拉角的定义、仿真算法库的建立等。
This paper deals with the numerical solution of the Euler equation for airfoils using approximate boundary conditions and the effects dorsal fin on vortex over delta wing at high angles of attack.
本论文主要是通过实验来研究细长圆锥体在大迎角下的绕流流场的特性和细长三角翼加背鳍后对前缘涡的影响，检验相关理论结果。
This paper deals with the numerical solution of the Euler equation for airfoils using approximate boundary conditions and the effects dorsal fin on vortex over delta wing at high angles of attack.
本论文主要是通过实验来研究细长圆锥体在大迎角下的绕流流场的特性和细长三角翼加背鳍后对前缘涡的影响，检验相关理论结果。
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