Coupled Oscillator: Double Pendulum: Difference between revisions

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Line 97: Line 97:
-\dfrac{8}{3} & 0 & \dfrac{2}{3}  & 0 \\
-\dfrac{8}{3} & 0 & \dfrac{2}{3}  & 0 \\
0            & 0 & 0            & 1 \\
0            & 0 & 0            & 1 \\
\dfrac{8}{8}  & 0 & -\dfrac{8}{3} & 0 \\
\dfrac{8}{3}  & 0 & -\dfrac{8}{3} & 0 \\
\end{bmatrix}
\end{bmatrix}



Revision as of 22:25, 11 December 2009

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−B20BEAD−B200001BCAD−B20−AEAD−B20]{θ1θ1'θ2θ2'}+0^

Let's plug some numbers. Knowing g=32, and assuming that m1=3, m2=1, and l1=l2=16, the constants defined previously become,

A=1024B=256C=2048D=256E=512

Hence, the state space matrix is,

[θ1'θ1'′θ2'θ2'′]=[0100−8302300001830−830]{θ1θ1'θ2θ2'}

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=[5s(5s2+8)25s4+80s2+128−5(5s2+8)25s4+80s2+128−40s25s4+80s2+1284025s4+80s2+1288(5s2+16)25s4+80s2+1285s(5s2+8)25s4+80s2+128−40s225s4+80s2+128−40s25s4+80s2+12840s25s4+80s2+128−4025s4+80s2+1285s(5s2+8)25s4+80s2+128−5(5s2+8)25s4+80s2+128−40s225s4+80s2+12840s25s4+80s2+1288(5s2+16)25s4+80s2+1285s(5s2+8)25s4+80s2+128]