“…J e : equivalent inertia including all rotating parts, : arm angle, M: equivalent mass of load and arm, g: gravitational constant, l: arm length, T h : operational torque by operator, T a : assist torque, T d : disturbance torque, n: gear ratio, K t : torque constant of motor, K : back emf constant, R: resistance, u: input voltage Using the state vector, x 4 [ 3 ] T , the state space model of the plan is represented by Considering a desired assist rate, maneuverability and so on, a desired closed-loop dynamics can be designed as follows (Yokoyama et al, 2006):…”