“…Local exponential stability) Given the model(7) of aerodynamic forces, consider the control system composed of the kinematic equations (1)-(2) and the Newton dynamic equation(8), augmented with the integrators (23) and (28). In the case of zero wind velocity and v * constant ( = 0), if the assumptions A1-A2 are satisfied and h * is a desired heading vector defined by (24)-(25), then the control inputs (T, ω) defined by(19),(21),(23) and (35) locally exponentially stabilize the equilibrium (p, v, B, z, I ev ) = (q, sign vu v * u,B, 0, 0).…”