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                       for inertial components, ii) Kirchhoff circuit laws for current-charge components, and iii) magnet circuit
                       laws for magnetic flux devices.
                         In this chapter we will examine the basic modeling assumptions for inertial, electric, and magnetic
                       circuits, which are typical of mechatronic systems, and will summarize the dynamic principles and
                       interactions between the mechanical motion, circuit, and magnetic state variables. We will also illustrate
                       these principles with a few examples as well as provide some bibliography to more advanced references
                       in electromechanics.

                       7.2 Models for Electromechanical Systems

                       The fundamental equations of motion for physical continua are partial differential equations (PDEs),
                       which describe dynamic behavior in both time and space. For example, the motions of strings, elastic
                       beams and plates, fluid flow around and through bodies, as well as magnetic and electric fields require
                       both spatial and temporal information. These equations include those of elasticity, elastodynamics, the
                       Navier–Stokes equations of fluid mechanics, and the Maxwell–Faraday equations of electromagnetics.
                       Electromagnetic field problems may be found in Jackson (1968). Coupled field problems in electric fields
                       and fluids may be found in Melcher (1980) and problems in magnetic fields and elastic structures may
                       be found in the monograph by Moon (1984). This short article will only treat solid systems.
                         Many practical electromechanical devices can be modeled by lumped physical elements such as mass
                       or inductance. The equations of motion are then integral forms of the basic PDEs and result in coupled
                       ordinary differential equations (ODEs). This methodology will be explored in this chapter. Where physical
                       problems have spatial distributions, one can often separate the problem into spatial and temporal parts
                       called  separation of variables. The spatial description is represented by a  finite number of spatial or
                       eigenmodes each of which has its modal amplitude. This method again results in a set of ODEs. Often
                       these coupled equations can be understood in the context of simple lumped mechanical masses and
                       electric and magnetic circuits.

                       7.3 Rigid Body Models


                       Kinematics of Rigid Bodies
                       Kinematics is the description of motion in terms of position vectors r, velocities v, acceleration a, rotation
                       rate vector ω, and generalized coordinates {q k (t)} such as relative angular positions of one part to another
                       in a machine (Fig. 7.1). In a rigid body one generally specifies the position vector of one point, such as
                       the center of mass r c , and the velocity of that point, say v c . The angular position of a rigid body is specified
                       by angle sets call Euler angles. For example, in vehicles there are pitch, roll, and yaw angles (see, e.g.,
                       Moon, 1999). The angular velocity vector of a rigid body is denoted by ω. The velocity of a point in a
                       rigid body other than the center of mass, r p  = r c  + ρ, is given by
                                                        v  = v  + ω × ρ                           (7.1)
                                                         P
                                                             c
                       where the second term is a vector cross product. The angular velocity vector w is a property of the entire
                       rigid body. In general a rigid body, such as a satellite, has six degrees of freedom. But when machine
                       elements are modeled as a rigid body, kinematic constraints often limit the number of degrees of freedom.

                       Constraints and Generalized Coordinates
                       Machines are often collections of rigid body elements in which each component is constrained to have
                       one degree of freedom relative to each of its neighbors. For example, in a multi-link robot arm shown
                       in Fig. 7.2, each rigid link has a revolute degree of freedom. The degrees of freedom of each rigid link
                       are constrained by bearings, guides, and gearing to have one type of relative motion. Thus, it is convenient

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