“…For simplicity, in this work only the motion in the local level plane is considered to illustrate and test the proposed scheme, which can be seen in Figure 2, where O ‐ XY is the inertial coordinates, o ‐ xy is body‐fixed coordinates. The 3‐DOF dynamic and kinematic equation of motion of an AUV can be written in the following form [
17]:
where η = [ x , y , ψ ] T denotes lateral motion, longitudinal and yaw angle of AUV and v = [ u , v , r ] T is made up of velocities in the three dimension; M = diag ( M u , M v , M r ) is inertial matrix with added mass; D ( v ) = diag( X u , Y v , N r ) + diag( D u | u |, D v | v |, D r | r |) is the damping matrix; restoring force is given by g ( η ); τ denotes generalized control input; τ d is vector of unknown disturbance; C ( v ) v represents the Coriolis and centripetal forces, and the coefficient matrix can be written as
…”