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[NOTES/CM-08006] Axis Angle Parametrization of Rotation Matrix

A closed form expression for rotation matrix is derived for rotations about an axis by a specified angle \(\theta\).

\begin{equation}
R_{\hat{n}}(\theta)=\widehat {Id}-\sin (\theta) (\hat{n}\cdot \vec{I})+(1-\cos \theta)(\hat{n}\cdot\vec{I})^{2}
\end{equation}Here  \(\widehat{Id} \) is the identity matrix. and \(\vec{I}=(I_1,I_2,I_3)\) is given by 
\begin{equation} I_1=\left[\begin{array}{clc} 0 &0 &0\\ 0 &0 &-1\\ 0 &1 &0 \end{array}\right],I_2=\left[\begin{array}{clc} 0 &0 &1\\ 0 &0 &0\\ -1 &0 &0 \end{array}\right],I_3=\left[\begin{array}{clc} 0 &-1 &0\\ 1 &0 &-1\\ 0 &1 &0 \end{array}\right] \end{equation}. 

Also the components of the position vector a point transform a

\begin{equation} {\vec{x}}\Prime=(\hat{n}\cdot{\vec{x}})\hat{n}+\cos\theta\big(\vec{x}-(\vec{x}\cdot\vec{n})\hat{n}\big)-\sin\theta (\hat{n}\times \vec{x})\end{equation}

 

kapoor's picture 24-06-17 22:06:34

[NOTES/CM-08004] Equation of Motion in Non Inertial Frames

 We derive an expression for Lagrangian for motion of a charged particle in a rotating frame, It is shown that the equation of motion can be written as

\begin{eqnarray} m\ddot{\vec{x}}=\vec{F_{e}}-2m\vec{\omega}\times{\dot{\vec{x}}}-m\vec{\omega} \times(\vec{\omega}\times\vec{x}) \end{eqnarray} where \(\vec {F}_e\) is the external force. As seen from the rotating frame, the particle moves as if it is under additional forces

  • $-2m\vec{\omega}\times{\dot{\vec{x}}}$ is called Coriolis force
  • $-m\vec{\omega}\times(\vec{\omega}\times\vec{x})$ is known as centrifugal force 

 

kapoor's picture 24-06-17 20:06:56

[NOTES/CM-08014] Active and Passive Rotations

The active and passive view of rotations are defined and relationship between them is described.

 

kapoor's picture 24-06-17 19:06:18

[NOTES/CM-08001] The Group of Special Orthogonal Matrices in \(N\) Dimensions

All  orthogonal  all \(N\times N\) orthogonal matrices  form a group called \(O(N)\). The set of all orthogonal  matrices with unit determinant  form a subgroup \(SO(N)\) . The group of all proper rotations coincides with \(SO(3)\).

kapoor's picture 24-06-16 15:06:35

[NOTES/CM-09010] A Heavy Top ---- Special Cases

A heavy top is a rigid body  moving under influence of gravity with one of its points fixed. A brief description of four interesting cases of a heavy top is given.

kapoor's picture 24-06-15 13:06:30

[NOTES/CM-09011] General Displacement of a Rigid Body

TO BE FINALIZED

kapoor's picture 24-06-15 12:06:35

[NOTES/CM-09009] General comments on Motion of a Rigid Body

We discuss some general questions about, choice of frames of reference, generalized coordinates and constants of motion.

 

TO BE FINALIZED

kapoor's picture 24-06-15 11:06:28

[NOTES/CM-09012] Why Two Sets, Body and Space Sets, of Axes?

The Newton's laws hold in an inertial  frame. However the equations of motion involve the moment of inertia tensor which in turn depends on the orientation of the body and varies with time. This make it solution to the motion of a rigid body  problem impossible. This difficulty is absent in the body fixed axes, the moment of inertia tensor depends only on the the geometry of the problem. So whether we use space axes ,or the body axes, depends on the problem to be solved, we use axes which makes the solution of the problem simpler.

kapoor's picture 24-06-15 11:06:41

[NOTES/CM-10012] Continuous Symmetry Transformation

In the phase space formulation, the constant of motion \(G\) given by Noether's theorem, expressed in terms of coordinates and momenta generates the infinitesimal symmetry transformation.

kapoor's picture 24-06-15 05:06:11

[NOTES/CM-10011] Infinitesimal Canonical Transformation

The definition of infnitesimal transformations is given.

kapoor's picture 24-06-15 05:06:01

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