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0593_C11_fm  Page 359  Monday, May 6, 2002  2:59 PM





                       Generalized Dynamics: Kinematics and Kinetics                               359


                       Observe that Eqs. (11.3.8), (11.3.9), and (11.3.10) constitute three constraint equations.
                       Hence, the disk D has three degrees of freedom, as expected. Observe next that the third
                       equation, Eq. (11.3.10), is integrable in terms of elementary functions. That is,

                                                          z = cosθ                             (11.3.11)
                                                             r
                       From Figure 11.3.1, we see that this expression is simply a requirement that D remains in
                       contact with the surface S — a geometric, or holonomic, constraint. Finally, observe that
                       Eqs. (11.3.8) and (11.3.9) are not integrable in terms of elementary functions. Instead, they
                       are coupled nonlinear differential equations requiring numerical solution. These expres-
                       sions arise from the requirement that C must have zero velocity in S — a kinematic, or
                       nonholonomic, constraint.
                        In the following and subsequent sections we will see that simple analyses using energy
                       functions (that is, the use of kinetic energy and Lagrange’s equations) are precluded with
                       nonholonomic systems. With Kane’s equations, however, the analysis is essentially the
                       same for both holonomic and nonholonomic systems. Nevertheless, our focus will be on
                       holonomic systems because, as noted earlier, the vast majority of mechanical systems of
                       interest are holonomic systems.






                       11.4 Vector Functions, Partial Velocity, and Partial Angular Velocity

                       Consider a holonomic mechanical system S having n degrees of freedom represented by
                       the coordinates q  (r = 1,…, n). Let P be a typical point of S. Then, a position vector p
                                      r
                       locating P relative to a fixed point O in an inertia frame R will, in general, be a function
                       of the q  and time t. That is,
                             r

                                                          p =  p(qt )                           (11.4.1)
                                                                 ,
                                                                r
                       Then, from the chain rule for differentiation, the velocity of P in R is:

                                                                  n
                                                    v =  d p  =  ∂ p + ∑  ∂ p  q ˙              (11.4.2)
                                                        dt   ∂t     ∂q  r
                                                                 r =1  r

                        The terms ∂p/∂t and ∂p/∂q  (r = 1,…, n) are called partial velocity vectors. These vectors
                                                 r
                       are fundamental vectors in the development of generalized dynamics theories and pro-
                       cedures. Indeed, they may be viewed as base vectors in the generalized space of motion
                       of a mechanical system. Because of their fundamental nature and widespread use, they
                       are given a separate notation defined as:

                                                    D
                                                  v = ∂ p t and  v = ∂ p q r                    (11.4.3)
                                                                        ∂
                                                         ∂
                                                                   D
                                                                  ˙
                                                   t
                                                                 q r
                       Then, from Eq. (11.4.2), we have:
                                                         v =∂  v q ˙                            (11.4.4)
                                                                 ∂
                                                           ˙ q r   r
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