Mahony, RobertHamel, Tarek2015-12-132015-12-131049-8923http://hdl.handle.net/1885/77948This paper considers the question of obtaining an a priori bound on the tracking performance, for an arbitrary trajectory, of closed-loop control of an idealized model of a scale model autonomous helicopter. The problem is difficult due to the presence of small body forces that cannot be directly incorporated into the control design. A control Lyapunov function is derived for an approximate model (in which the small body forces are neglected) using backstepping techniques. The Lyapunov function derived is used to analyse the closed-loop performance of the full system. A theorem is proved that provides a priori bounds on initial error and the trajectory parameters (linear acceleration and its derivatives) that guarantees acceptable tracking performance of the system. The analysis is expected to be of use in verification of trajectory planning procedures.Keywords: Approximation theory; Closed loop control systems; Lyapunov methods; Nonlinear control systems; Problem solving; Robustness (control systems); Theorem proving; Autonomous helicopters; Lyapunov control design; Robustness analysis; Helicopters Autonomous helicopters; Lyapunov control design; Nonlinear system; Robustness analysis200410.1002/rnc.9312015-12-11