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A novel three-dimensional law based on input-to-state stability (ISS) and nonlinear robust H∞ filtering is proposed for interception of maneuvering targets in the presence of input saturation. A dead zone operator model is introduced to design an ISS-based guidance law to guarantee robust tracking of a maneuvering target. Input saturation and system stability are considered simultaneously, and the...
Hypersonic vehicles are near space vehicle with high Mach number. This paper considers the general hypersonic longitudinal model with uncertainties. According to the characteristics of the longitudinal model, it can be divided into two independent parts, i.e., the speed control channel and the altitude control channel. In the altitude control channel, backstepping is used to design a control law such...
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