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3-DOF motion of spherical actuator. (a) First tilting motion. (b) Second tilting motion. (c) Spinning motion.  

3-DOF motion of spherical actuator. (a) First tilting motion. (b) Second tilting motion. (c) Spinning motion.  

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Article
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This paper has proposed a 3-DOF spherical actuator consisting of a ball-shaped rotor with a full circle of permanent- magnet (PM) poles and a spherical-shell-like stator with two layers of circumferential air-core coils. One key feature of this design is the parametrization of PM and coil poles. Based on the torque model of the PM spherical actuato...

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... working principle of this spherical actuator is illustrated in Fig. 1. This spherical actuator consists of a ball-shaped rotor with a full circle of PM poles and a spherical-shell-like stator with two layers of circumferential air-core coils. The rare earth PMs can generate high flux density within the actuator, and the air-core coils may simplify the torque model in a linear fash- ion. With pairs of ...
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... stator with two layers of circumferential air-core coils. The rare earth PMs can generate high flux density within the actuator, and the air-core coils may simplify the torque model in a linear fash- ion. With pairs of coils activated in two longitudinal directions, the rotor creates tilting motions in two orthogonal directions as shown in Fig. 1(a) and (b). By energizing the rest of the circumferential coils, the rotor can spin about its axis. There- fore, through varying the current input of coils, the actuator can produce any desirable 3-DOF rotational motion within the ...
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... packing pattern of winding affects the number of wire turns placed within a given area. Fig. 10(a) illustrates the regular packing pattern and Fig. 10(b) is the staggering pattern. The density of the patterns can be computed and compared for their effectiveness. Here, the stacking density is defined as the ratio of the occupied cross- sectional area of the wires and that of the designated square space (Fig. 10). For the regular ...
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... packing pattern of winding affects the number of wire turns placed within a given area. Fig. 10(a) illustrates the regular packing pattern and Fig. 10(b) is the staggering pattern. The density of the patterns can be computed and compared for their effectiveness. Here, the stacking density is defined as the ratio of the occupied cross- sectional area of the wires and that of the designated square space (Fig. 10). For the regular pattern, the stacking density ...
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... placed within a given area. Fig. 10(a) illustrates the regular packing pattern and Fig. 10(b) is the staggering pattern. The density of the patterns can be computed and compared for their effectiveness. Here, the stacking density is defined as the ratio of the occupied cross- sectional area of the wires and that of the designated square space (Fig. 10). For the regular pattern, the stacking density ...
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... Reduction of Wire Diameter: Wire diameter affects the number of winding turns. Generally, small diameter of wires allows more turns of winding to occupy the same area. Analysis is carried out to estimate the increased coil turns due to diameter reduction of wires. Based on Fig. 11, the number of turns that occupies the sectional area can be computed ...
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... on the aforesaid analysis, a research prototype of the actuator has been developed (Fig. 12). The specification is listed in Table II. Eight PM poles are mounted along the rotor equator. Twenty-four circumferential holes are drilled through the stator shell and arranged in two layers symmetrically about the stator equator. Coils are mounted through these holes and point to the stator center. The threads in the holes allow coil ...
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... the assembly of the spherical actuator, it is required that the rotor is concentric with the stator. Two cylindrical holes separated 90 • apart are drilled at the stator equator plane, as shown in Fig. 13. Likewise, two holes that are separated 90 • apart and pointed to the rotor center are drilled at the rotor equator plane. Two centering pins can be inserted through the holes on the stator shell to the holes on the rotor. In this way, the concentricity of the rotor and the stator can be ...
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... is housed within the stator directly. Although a low friction coating was made on the stator inner surface, the sliding friction between the rotor and the stator might cause unfavorable effect on the rotor motion. In some spherical motors [5], [9], transfer bearings or analog are used to support the rotor. A typical transfer bearing is shown in Fig. 14(a). This bearing consists of a rolling ball on the top, which can create a rolling motion with respect to the contact sur- face. The screw on the other end can fix the bearing on the stator for adjusting its position. As indicated in Fig. 14(b), to support a spherical rotor stably, at least three transfer bearings are nec- essary. The ...
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... [9], transfer bearings or analog are used to support the rotor. A typical transfer bearing is shown in Fig. 14(a). This bearing consists of a rolling ball on the top, which can create a rolling motion with respect to the contact sur- face. The screw on the other end can fix the bearing on the stator for adjusting its position. As indicated in Fig. 14(b), to support a spherical rotor stably, at least three transfer bearings are nec- essary. The rolling motion of these transfer bearings produces rolling frictions lower than the sliding frictions. Nevertheless, the friction torque from the transfer bearing relative to the rotor center is large due to the rotor radius. The nonnegligible ...
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... our spherical actuator, a spherical bearing [ Fig. 15(a)] [16] is employed to support the rotor housed in the stator. This spher- ical bearing can achieve a smooth 3-DOF rotational motion. The tilting motion range of this bearing is up to ±35 • . It can be as- sembled at the rotor center, as shown in Fig. 15(b). Because the friction produced by this spherical bearing is very small and the ...
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... our spherical actuator, a spherical bearing [ Fig. 15(a)] [16] is employed to support the rotor housed in the stator. This spher- ical bearing can achieve a smooth 3-DOF rotational motion. The tilting motion range of this bearing is up to ±35 • . It can be as- sembled at the rotor center, as shown in Fig. 15(b). Because the friction produced by this spherical bearing is very small and the moment arm of the friction force is less than 4 mm, the friction torque produced by the spherical bearing is negligible. Com- pared with the air bearing, the implementation of this spherical bearing is also ...
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... workspace of the PM spherical actuator is shown in Fig. 16(a). A series of PM poles are mounted along the rotor equator, whereas the air-core coils are symmetrically mounted on the stator with respect to the stator equatorial plane, with two layers separated by an angular distance of θ s . The rotor shaft can spin about its own z-axis, Z r , in 360 • without constraint. It can also incline to an ...
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... plane, with two layers separated by an angular distance of θ s . The rotor shaft can spin about its own z-axis, Z r , in 360 • without constraint. It can also incline to an extreme position that the axes of a PM pole and the coil are aligned. Thus, the z-axis of the rotor can move within a conical workspace with a conical angle of θ s as shown in Fig. ...
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... orientation of the rotor frame with respect to the stator frame can be expressed by using Euler angles. Let the rotor frame be (X r , Y r , Z r ) and the stator frame be (X s , Y s , Z s ). In order to arrive at an arbitrary final orientation within the workspace, three rotor rotations have to take place in sequence [ Fig. 16(b)]. The Euler ZYZ angle expression of the rotor orien- tation can be written as the multiplication of three body rotation matrices R z (φ r ), R y (θ r ), and R z (δ r ) [21] ...
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... computing process of torque matrix Q from the rotor orientation is carried out as follows (Fig. ...
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... of the condition numbers can be visualized. By fixing φ r at certain values such as 0 • , 15 • , 30 • , etc., a 3D plot of the condition number, denoted as n c , with respect to the variation of θ r and δ r can be presented visually as a 2-D surface. By choosing different φ r , a set of 2-D surfaces can be obtained, some of which are shown in Fig. 18. Due to the symmetric arrangement of the PM poles about the shaft, only the ranges of φ r = 0 • -45 • and δ r = 0 • -45 • are considered. Referring to Fig. 18, we can find that the condition numbers n c do not vary too much with respect to δ r and φ r because of the evenly distributed PM poles along the rotor equator. It can also be ...
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... n c , with respect to the variation of θ r and δ r can be presented visually as a 2-D surface. By choosing different φ r , a set of 2-D surfaces can be obtained, some of which are shown in Fig. 18. Due to the symmetric arrangement of the PM poles about the shaft, only the ranges of φ r = 0 • -45 • and δ r = 0 • -45 • are considered. Referring to Fig. 18, we can find that the condition numbers n c do not vary too much with respect to δ r and φ r because of the evenly distributed PM poles along the rotor equator. It can also be found that the minimum value of the condition number is 4.877, whereas the maximum value is 5.145, which is of the same order of magnitude 1. Therefore the ...

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... where Ns is the number of parallel winding strands, Dw is the wire diameter, dl is the thickness of insulation layer, ρw is the wire resistivity, Rin and Rout are the inner and outer radius of the coil, respectively, dc is the thickness of the coil, and ρd is wire stacking density which can be described as [48] 2 2 ...
... The second type is the complete spherical geometry, which is actuated by external actuators in contact with the surface of the sphere. This design was reported in [29][30][31]. Another design based on this principle was presented in [32], where a pair of sliced orthogonal wheels were placed perpendicularly on the axle. ...
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... The magnetically suspended RSA has a single spherical rotor that can rotate in any direction with spherical angular momentum storage production capability [7,8]. Magnetically suspended RSA produces high torque due to tilting capability of sphere and the vibration is less than other conventional actuators such as the reaction wheel, thruster, and magnetorquer utilizing a magnetic-based mechanism such as a permanent magnet [9], electromagnetic induction [10], and piezo and ultrasonic motors [11]. ...
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Next, the motors’ state-space description undergoes approximate linearization with the use of first-order Taylor series expansion and through the computation of the associated Jacobian matrices. The linearization process takes place at each sampling instance around a time-varying operating point, which is defined by the present value of the motors’ state vector and by the last sampled value of the control input vector. For the approximately linearized model of the permanent magnet synchronous spherical motors, a stabilizing H-infinity feedback controller is designed. To compute the controller’s gains, an algebraic Riccati equation has to be repetitively solved at each time-step of the control algorithm. The global stability properties of the control scheme are proven through Lyapunov analysis. Finally, the performance of the nonlinear optimal control method is compared against a flatness-based control approach implemented in successive loops. Findings Due to the nonlinear and multivariable structure of the state-space model of spherical motors, the solution of the associated nonlinear control problem is a nontrivial task. In this paper, a novel nonlinear optimal (H-infinity) control approach is proposed for the dynamic model of permanent magnet synchronous spherical motors. The method is based on approximate linearization of the motor’s state-space model with the use of first-order Taylor series expansion and the computation of the associated Jacobian matrices. Furthermore, the paper has introduced a different solution to the nonlinear control problem of the permanent magnet synchronous spherical motor, which is based on flatness-based control implemented in successive loops. Research limitations/implications The presented control approaches do not exhibit any limitations, but on the contrary, they have specific advantages. In comparison to global linearization-based control schemes (such as Lie-algebra-based control), they do not make use of complicated changes of state variables (diffeomorphisms) and transformations of the system's state-space description. The computed control inputs are applied directly to the initial nonlinear state-space model of the permanent magnet spherical motor without the intervention of inverse transformations and thus without coming against the risk of singularities. Practical implications The motion control problem of spherical motors is nontrivial because of the complicated nonlinear and multivariable dynamics of these electric machines. So far, there have been several attempts to apply nonlinear feedback control to permanent magnet-synchronous spherical motors. However, due to the model’s complexity, few results exist about the associated nonlinear optimal control problem. The proposed nonlinear control methods for permanent magnet synchronous spherical motors make more efficient, precise and reliable the use of such motors in robotics, electric traction and several automation systems. Social implications The treated research topic is central for robotic and industrial automation. Permanent magnet synchronous spherical motors are suitable for several applications, such as actuation in robotics, traction in electric vehicles and use in several automation systems. The solution of the control problem for the nonlinear dynamic model of permanent magnet synchronous spherical motors has many industrial applications and therefore contributes to economic growth and development. Originality/value The proposed nonlinear optimal control method is novel compared to past attempts to solve the optimal control problem for nonlinear dynamical systems. Unlike past approaches, in the new nonlinear optimal control method, linearization is performed around a temporary operating point, which is defined by the present value of the system's state vector and by the last sampled value of the control inputs vector and not at points that belong to the desirable trajectory (setpoints). Besides, the Riccati equation which is used for computing the feedback gains of the controller is new, and so is the global stability proof for this control method. Compared to nonlinear model predictive control, which is a popular approach for treating the optimal control problem in industry, the new nonlinear optimal (H-infinity) control scheme is of proven global stability, and the convergence of its iterative search for the optimum does not depend on initial conditions and trials with multiple sets of controller parameters. It is also noteworthy that the nonlinear optimal control method is applicable to a wider class of dynamical systems than approaches based on the solution of state dependent Riccati equations (SDRE). The SDRE approaches can be applied only to dynamical systems which can be transformed into the linear parameter varying form. Besides, the nonlinear optimal control method performs better than nonlinear optimal control schemes, which use approximation of the solution of the Hamilton–Jacobi–Bellman equation by Galerkin series expansions. Furthermore, the second control method proposed in this paper, which is flatness-based control in successive loops, is also novel and demonstrates substantial contribution to nonlinear control for robotics and industrial automation.
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