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The paper proposes a robust guidance law with high-order sliding mode variable structure to handle the problems of poor convergence and the control chattering variable structure considering limited guidance information when the target is suffering the high maneuver interception. A sliding surface is illustrated with finite time convergence. The high-order sliding mode variable structure guidance law...
In this brief, a fast robust integrated guidance and control design approach, considering the 3-D interception of interceptors for hypersonic vehicles, is proposed. The proposed method is designed using the modified fast terminal sliding mode control and dynamic surface control with signal compensation. The fractional integral fast terminal sliding functions are presented independently, and all the...
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