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相关概念视频

Equation of Motion for a Rigid Body01:12

Equation of Motion for a Rigid Body

238
The movement of a rigid object can be understood through the equations that explain both translational and rotational motion about the center of mass of the object, point G. This center of mass is the point where the equation of motion for translational motion comes into play, as per Newton's Second Law.
The combined moments generated about the center of mass of the object are equal to the rate of change of the angular momentum of the body. An external force, when applied at a different...
238
Euler Equations of Motion01:19

Euler Equations of Motion

188
Imagine a rigid body that is rotating at an angular velocity of ω within an inertial frame of reference. Along with this, picture a second rotating frame that is attached to the body itself. This frame moves along with the body and possesses an angular velocity of Ω. The total moment about the center of mass is calculated by adding the rate of change of angular momentum about the center of mass in relation to the rotating frame and the cross-product of the body's angular velocity...
188
Euler's Equations of Motion01:28

Euler's Equations of Motion

168
In fluid mechanics, shear stresses arise from viscosity, which represents a fluid's internal resistance to deformation. For low-viscosity fluids, like water, these stresses are minimal, simplifying flow analysis by allowing the fluid to be treated as inviscid, or frictionless. In an inviscid fluid, shear stresses are absent, leaving only normal stresses, which act perpendicularly to fluid elements. Notably, pressure — defined as the negative of the normal stress — remains...
168
Relative Motion Analysis using Rotating Axes01:25

Relative Motion Analysis using Rotating Axes

433
Consider a component AB undergoing a linear motion. Along with a linear motion, point B also rotates around point A. To comprehend this complex movement, position vectors for both points A and B are established using a stationary reference frame.
However, to express the relative position of point B relative to point A, an additional frame of reference, denoted as x'y', is necessary. This additional frame not only translates but also rotates relative to the fixed frame, making it...
433
Relative Motion Analysis using Rotating Axes-Problem Solving01:29

Relative Motion Analysis using Rotating Axes-Problem Solving

369
Consider a crane whose telescopic boom rotates with an angular velocity of 0.04 rad/s and angular acceleration of 0.02 rad/s2. Along with the rotation, the boom also extends linearly with a uniform speed of 5 m/s. The extension of the boom is measured at point D, which is measured with respect to the fixed point C on the other end of the boom. For the given instant, the distance between points C and D is 60 meters.
Here, in order to determine the magnitude of velocity and acceleration for point...
369
Kinematic Equations for Rotation01:30

Kinematic Equations for Rotation

294
In mechanics, when one observes a rigid body in rotational motion with constant angular acceleration, it is possible to establish equations for its rotational kinematics. This process resembles how linear kinematics are dealt with in simpler motion studies.
For instance, imagine a point A on a rigid body engaged in circular motion. The translational velocity of this particular point can be calculated by taking the time derivatives of the displacement equation, which essentially measures the...
294

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Updated: May 9, 2025

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基于欧勒参数的刚性-柔性合航天器的动态分析.

Yi Ji1,2,3, Huan Zhang4

  • 1School of Astronautics, Harbin Institute of Technology, Harbin, 150001, China.

Scientific reports
|May 3, 2025
PubMed
概括

这项研究引入了一种用于分析航天器动态的新数值方法. 加强了刚性-灵活合的BN稳定方法,为复杂的航空航天模拟提供了卓越的准确性和稳定性.

关键词:
在BN的稳定性.动态分析 动态分析欧勒参数 的参数.刚性-灵活的合器旋转矩阵是一个旋转矩阵.

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Author Spotlight: Development of a Novel Finite Element Analysis Model for Improved Orthognathic Surgical Techniques
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科学领域:

  • 航空航天工程 航空航天工程
  • 计算力学 计算力学 计算力学
  • 非线性动力学是一种非线性动力学.

背景情况:

  • 现代航天器具有复杂的刚性-柔性合,对动态分析构成重大挑战.
  • 现有的数值工具与这些系统固有的强烈非线性作斗争.

研究的目的:

  • 开发一种准确和高效的数值方法来分析刚性-柔性合航天器的动态行为.
  • 解决当前工具在处理高度非线性动态系统方面的局限性.

主要方法:

  • 描述了使用欧勒参数来避免单一角度的刚性和柔性物体.
  • 应用了重新设计的BN-stable方法,确保非线性初始值问题的无条件稳定性.
  • 整合了角速度-欧勒参数关系和速度级限制,以保持数值旋转矩阵的准确性.

主要成果:

  • 拟议的战略有效地模拟了航天器的动态反应,包括刚性物体和灵活的太阳翼.
  • 与现有的流行的策略相比,在准确性,稳定性和消散性方面表现出相当大的优势.
  • 验证了非线性系统的过渡响应分析的增强BN稳定方法.

结论:

  • 重构的BN-稳定方法为分析刚性-灵活合航天器动态提供了强大而准确的解决方案.
  • 这种方法克服了与航空航天模拟中的强烈非线性相关的关键挑战.
  • 与航天器动态分析的传统方法相比,提供了显著的改进.