Coupled Oscillator: Double Pendulum: Difference between revisions

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</math>
</math>
Let's plugs some numbers. Knowing <math>g (32)</math>, and assuming that <math>m_1=3</math>, <math>m_2=1</math>, and <math>l_1=l_2=16</math>, the state space matrix is,


=== Laplace Transform ===
=== Laplace Transform ===
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s                  & 1 & 0                  & 0 \\
s                  & 1 & 0                  & 0 \\
  & & & \\
  & & & \\
\dfrac{-CD}{AD+B^2} & s & \dfrac{-BE}{AD+B^2} & 0 \\
\dfrac{-8}{5} & s & \dfrac{-8}{5} & 0 \\
  & & & \\
  & & & \\
0                  & 0 & s                  & 1 \\
0                  & 0 & s                  & 1 \\
  & & & \\
  & & & \\
\dfrac{BC}{AD+B^2}  & 0 & \dfrac{-AE}{AD+B^2} & s \\
\dfrac{8}{5}  & 0 & \dfrac{-8}{5} & s \\
\end{bmatrix}
\end{bmatrix}


</math>
</math>


Hence, the inverse matrix is,  
Hence, the inverse matrix (thanks TI-89!) is,  


: <math>
: <math>
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s                  & 1 & 0                  & 0 \\
s                  & 1 & 0                  & 0 \\
  & & & \\
  & & & \\
\dfrac{-CD}{AD+B^2} & s & \dfrac{-BE}{AD+B^2} & 0 \\
\dfrac{-8}{5}       & s & \dfrac{-8}{5}       & 0 \\
  & & & \\
  & & & \\
0                  & 0 & s                  & 1 \\
0                  & 0 & s                  & 1 \\
  & & & \\
  & & & \\
\dfrac{BC}{AD+B^2} & 0 & \dfrac{-AE}{AD+B^2} & s \\
\dfrac{8}{5}       & 0 & \dfrac{-8}{5}       & s \\
\end{bmatrix}
\end{bmatrix}


</math>
</math>

Revision as of 13:39, 9 December 2009

By Jimmy Apablaza By Jimmy Apablaza

This problem is described in Page 321-322, Section 7.6 of the A first Course in Differential Equations textbook, 8ED (ISBN 0-534-41878-3).

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Figure 1. Coupled Pendulum.‎

Problem Statement

Consider the double-pendulum system consisting of a pendulum attached to another pendulum shown in Figure 1.

Assumptions:

  • the system oscillates vertically under the influence of gravity.
  • the mass of both rod are neligible
  • no dumpung forces act on the system
  • positive direction to the right.

The system of differential equations describing the motion is nonlinear

(m1+m2)l12θ1′′+m2l1l2θ2′′cos(θ1−θ2)+m2l1l2(θ2′)2sin(θ1−θ2)+(m1+m2)l1gsinθ1=0
m2l12θ2′′+m2l1l2θ1′′cos(θ1−θ2)−m2l1l2(θ1′)2sin(θ1−θ2)+m2l2gsinθ2=0


In order to linearize these equations, we assume that the displacements θ1 and θ2 are small enough so that cos(θ1−θ2)≈1 and sin(θ1−θ2)≈0. Thus,

(m1+m2)l12θ1′′+m2l1l2θ2′′+(m1+m2)l1gθ1=0
m2l12θ2′′+m2l1l2θ1′′+m2l2gθ2=0

Solution

Since our concern is about the motion functions, we will assign the masses m1 and m2, the rod lenghts l1 and l1, and gravitational force g constants to different variables as follows,

A=(m1+m2)l12B=m2l1l2C=(m1+m2)l1gD=m2l12E=m2l2g

Hence,

Aθ1'′+Bθ2'′+Cθ1=0
Dθ2'′+Bθ1'′+Eθ2=0

Solving for θ1'′ and θ2'′ we obtain,

θ1'′=−(BA)θ2'′−(CA)θ1
θ2'′=−(BD)θ1'′−(ED)θ2

Therefore,

θ1'′=−(CDAD+B2)θ1−(BEAD+B2)θ2
θ2'′=(BCAD+B2)θ1−(AEAD+B2)θ2

State Space

[θ1'θ1'′θ2'θ2'′]=A^x_(t)+B^u_(t)=[0100−CDAD+B20−BEAD+B200001BCAD+B20−AEAD+B20]{θ1θ1'θ2θ2'}+0^

Plugging the constants yields,

[θ1'θ1'′θ2'θ2'′]=[0100−l1(m1+m2)gl12(m1+m2)+l22m20−l22m2gl1(l12(m1+m2)+l22m2)00001l2(m1+m2)gl12(m1+m2)+l22m20−l2(m1+m2)gl12(m1+m2)+l22m20]{θ1θ1'θ2θ2'}

Let's plugs some numbers. Knowing g(32), and assuming that m1=3, m2=1, and l1=l2=16, the state space matrix is,

Laplace Transform

First, we determine the eigenvalues of the A^ matrix,

[sI−A]=[s100−85s−85000s1850−85s]

Hence, the inverse matrix (thanks TI-89!) is,

[sI−A]−1=[s100−85s−85000s1850−85s]