Boundary Control of a Quadrotor UAV with a Payload Connected by a Flexible Cable

This paper addresses the problem of boundary control design for a quadrotor UAV with a payload connected by a flexible cable. The extend Hamilton's principle is applied to establish the model of the slung-load system which consists of two nonlinear wave equations. The objective of this paper is to design boundary feedback controllers for the slung-load system via the cable's boundary measurements such that the resulting closed-loop system is exponentially stable. The Lyapunov's direct method is employed to derive the stabilization condition for the system, which is provided in terms of linear matrix inequalities (LMIs). The numerical simulation illustrates the effectiveness of the proposed design method.

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