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0593_C12_fm  Page 433  Monday, May 6, 2002  3:11 PM





                       Generalized Dynamics: Kane’s Equations and Lagrange’s Equations             433


                       to Eqs. (8.11.1), (8.11.2), and (8.11.3) reportedly developed using d’Alembert’s principle.
                       Although the details of that development were not presented, the use of Lagrange’s
                       equations has the clear advantage of providing the simpler analysis. As noted before, the
                       simplicity and efficiency of the Lagrangian analysis stem from the avoidance of the
                       evaluation of accelerations and from the automatic elimination of nonworking constraint
                       forces. In the following section, we outline the extension of this example to include N rods.







                       12.5 The N-Rod Pendulum
                       Consider a pendulum system composed of N identical pin-connected rods with a point
                       mass Q at the end as in Figure 12.5.1 (we considered this system [without the end mass]
                       in Section 8.11). As before, let each rod have mass m and length  . Also, let us restrict our
                       analysis to motion in the vertical plane. The system then has  N degrees of freedom
                       represented by the angles θ  (i = 1,…, n) as shown in Figure 12.5.1. This system is useful
                                               i
                       for modeling the dynamic behavior of chains and cables.
                        We can study this system by generalizing our analysis for the triple-rod pendulum.
                       Indeed, by examining Eqs. (12.4.1) through (12.4.10), we see patterns that can readily be
                       generalized. To this end, consider a typical rod  B  as in Figure 12.5.2. Then, from Eq.
                                                                    i
                       (12.4.1), the angular velocity of B  in the fixed inertia frame may be expressed as:
                                                    i
                                                               ˙
                                                          ωω = θ n                             (12.5.1)
                                                            B 1
                                                                i  3
                       where n  is a unit vector normal to the plane of motion as in Figure 12.5.2.
                              3
                        Next, from Eq. (12.4.2), the velocity of the mass center G  may be expressed as:
                                                                           i
                                                 n + lθ
                                          v = lθ ˙  11 θ  ˙  2 n +…+ lθ ˙  i−1 n  i− ( 1 )θ  +(l 2  ˙ i )θ  n iθ  (12.5.2)
                                           G i
                                                          θ
                                                          2
                       where as before, and as in Figure 12.5.2, the n  are unit vectors normal to the rods.
                                                                iθ
                        Similarly, the velocity of the point mass Q is:
                                                       n + lθ
                                                v = lθ ˙  11 θ  ˙  2 n +…+ lθ ˙  N n Nθ        (12.5.3)
                                                 Q
                                                                θ
                                                                2

                         θ                                                    n  iθ
                          1
                               θ
                             2
                                                                                              n
                                   θ 3                                                         3
                                                                                    n
                                                                       θ i           ir
                                                                              G
                                          θ    n-1   Q(M)                       i
                                               θ   n                                   B  i

                       FIGURE 12.5.1                                 FIGURE 12.5.2
                       N-rod pendulum with endpoint mass.            A typical rod of the pendulum.
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