Output feedback continuous terminal sliding mode guidance law for missile-target interception with autopilot dynamics

This paper proposes an output feedback continuous terminal sliding mode guidance law (CTSMGL) for three-dimensional missile-target interception with consideration of second-order autopilot dynamics. The proposed output feedback CTSMGL not only guarantees the rates of the line-of-sight angles converge to zero in finite time but also ensures the continuity of control action. Besides, only the relative range and velocity information of guidance...