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0593_C12_fm  Page 429  Monday, May 6, 2002  3:11 PM





                       Generalized Dynamics: Kane’s Equations and Lagrange’s Equations             429


                       By substituting from Eqs. (12.3.15), (12.3.17), (12.3.18), (12.3.19), and (12.3.20), the govern-
                       ing equations become:


                                              mx ˙˙ −  m(l + x )θ ˙ 2  = mgcos + kx −  2 kx   (12.3.32)
                                                                    θ
                                                1        1               2    1
                                                   m 2 + )θ
                                                                     θ
                                             mx ˙˙ − ( l  x  ˙ 2  =  mgcos +  kx +  kx        (12.3.33)
                                                2         2               3    1
                                                                     θ
                                                  m 3 + )θ
                                             mx ˙˙ − ( l  x  ˙ 2  = mgcos −  2 kx +  kx       (12.3.34)
                                               3         3                 3   2
                       and
                                            [
                                                                      ]
                                          m l + (  x ) +(2 l +  x ) +(3 l + x ) θ  +( ) 3  ML θ
                                                                     2
                                                            2
                                                  2
                                                                                 2 ˙˙
                                                                       ˙˙
                                                                          1
                                                 1
                                                          2
                                                                    3
                                              m l + ( [                    x x ) ]
                                                                  ˙
                                                      ˙
                                             + 2   x x ) θ ˙  +(2 l + x x ) θ ˙  +(3 l +  ˙ θ ˙  (12.3.35)
                                                    1  1        2  2        3  3
                                              =− Mg L ( ) 2 sinθ − mg l + x + x + )sinθ
                                                              (6
                                                                          x
                                                                           3
                                                                    1
                                                                       2
                        Equations (12.3.22), (12.3.23), (12.3.24), and (12.3.25) are seen to be identical to Eqs.
                       (12.2.32), (12.2.33), (12.2.34), and (12.2.35) obtained using Kane’s equations.
                       12.4 The Triple-Rod Pendulum
                       As a further illustration of the use of Lagrange’s equations, consider the triple-rod pen-
                       dulum depicted in Figure 12.4.1. We initially considered this system in Section 8.11. As
                       before, let the three rods be identical, each having length   and mass m. Let the rods be
                       connected by frictionless pins. As a generalization of the system of Section 8.11, however,
                       let there be moments M , M , and M  on and between the rods as in Figure 12.4.1. Also,
                                            1   2      3
                       let there be a point mass Q (with mass M) at the end of the third rod as shown. This
                       system has three degrees of freedom as represented by the angles θ  , θ  , and θ .
                                                                                   1   2      3
                        To develop the kinematics it is helpful to introduce the unit vectors and points shown
                       in Figure 12.4.2, where G , G , and G  are the mass centers of the rods, O, Q , and Q  are
                                             1  2      3                                   1      2
                                                                              n  1  θ
                             M  1                                 O                              n  2
                                                                                  n  2    θ
                                                                            n          n  3     θ  n  1
                                                                      G  1   1 r
                          θ                                         θ
                            1     M  2                               1    Q  1   n  2 r
                                                                             G  2
                                           M                                                  n  3 r
                                   θ        3                                θ    Q  2
                                  2                                        2           G  3
                                          θ                                        θ
                                             3    Q                                   3    Q
                                                                      n
                                                                        3
                       FIGURE 12.4.1                            FIGURE 12.4.2
                       A triple-rod pendulum.                   Unit vector geometry.
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