“…As in the case of the levitation stiffness, the fluctuation in this guidance force is almost sinusoidal, and this component can also be expressed as an approximate equation. From Figure 13, the maximum, average, and minimum values of the guidance stiffness with respect to the lateral position can be expressed as a quadratic function for Designs A, B, and C, as expressed in Equations ( 22)-( 30 From Figure 13, the maximum, average, and minimum values of the guidance stiffness with respect to the lateral position can be expressed as a quadratic function for Designs A, B, and C, as expressed in Equations ( 22)-( 30) [21,[25][26][27][28][29]. Here, the unit is N/m.…”