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0593_C08_fm  Page 264  Monday, May 6, 2002  2:45 PM





                       264                                                 Dynamics of Mechanical Systems



















                       FIGURE 8.12.1                            FIGURE 8.12.2
                       Rotating, pinned rod.                    Unit vectors of the shaft and rod.
                       line of S. Let B have length   and mass m, and let the orientation of B be defined by the
                       angle θ as shown in Figure 8.12.1.
                        We can obtain the equation governing θ and, hence, the motion of B by proceeding as
                       in the previous examples. To this end, consider first the kinematics of B: Let unit vectors
                       n , n , n , n , and n  be introduced as in Figure 8.12.2, where n  is parallel to the pin axis
                        1  2  3  r      θ                                      r
                       of B and radial line of S; n  is perpendicular to k and n ; and n , n , and n  are mutually
                                              θ
                                                                               1
                                                                        r
                                                                                         3
                                                                                  2
                       perpendicular dextral unit vectors, with n  being parallel to n  and n  being along B, as
                                                             3                 r     1
                       shown. Then, these unit vectors are related to each other by the expressions:
                                                     n =−cosθ k + sinθ n θ
                                                      1
                                                     n = sinθ k + cosθ n θ                     (8.12.1)
                                                      2
                                                     n =  n r
                                                      3
                       and
                                                     n =  n
                                                      r   3
                                                     n = sin θ n + cos θ n 2                   (8.12.2)
                                                      θ
                                                              1
                                                     k =−cos θ n + sin θ n
                                                               1       2
                       The angular velocity ωω ωω of B in the inertia frame R in which S is rotating may be obtained
                       using the addition theorem for angular velocity (see Section 4.7). That is,

                                                                 Ω
                                                         ωω= θn  + k                           (8.12.3)
                                                              r
                       Then, by differentiating, we obtain the angular acceleration of B as:


                                                                     ˙
                                                         ˙˙
                                                              ˙
                                                               Ω
                                                                    Ω
                                                      αα= θn  r  + θ n θ  + k                  (8.12.4)
                       By using Eqs. (8.12.2) ωω ωω and αα αα may be expressed in terms of n , n , and n  as:
                                                                              1  2      3
                                                                         ˙
                                                 ωω= −Ωcosθn  + Ωsinθn  + θn                   (8.12.5)
                                                             1        2    3
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