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- W4386483758 abstract "Distributed adaptive cooperative guidance problem for multiple missiles intercepting a maneuvering target with time-varying terminal angle constraint and overload saturation is investigated in this paper. First of all, an extended state observer (ESO) is designed for each missile which can estimate the line-of-sight (LOS) rate and unknown external disturbances simultaneously. Secondly, a sliding manifold is proposed for each missile which consists of states of the ESO and neighbor terminal angle formation error. Then, a distributed cooperative guidance law is presented which can achieve the terminal angle constrained cooperative guidance. Furthermore, in order to deal with overload saturation, an auxiliary state is designed for the stability of the whole guidance system. Thirdly, the design process of cooperative guidance law is summarized as a guidance algorithm and the stability of the guidance error dynamics is proved via Lyapunov theories. Finally, the validity of the presented cooperative guidance algorithm is demonstrated by a numerical example." @default.
- W4386483758 created "2023-09-07" @default.
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- W4386483758 date "2023-11-01" @default.
- W4386483758 modified "2023-10-15" @default.
- W4386483758 title "Distributed adaptive cooperative guidance against maneuvering targets with time-varying terminal angle constraint and overload saturation" @default.
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- W4386483758 doi "https://doi.org/10.1016/j.jfranklin.2023.08.041" @default.
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