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- W2834329510 abstract "With multiple path constraints taken into consideration during hypersonic glide phase, a new sliding mode tracking guidance based on three-dimensional trajectory is proposed. Firstly, on the basis of entry vehicle dynamics and geometrical transformation, the dynamics formulation of crossrange parameter is derived. Therefore, a nonlinear guidance model composed of crossrange parameter and flight path angle is formed. Secondly, with the aid of feedback linearization technology, the nonlinear dynamics equations are converted into linear ones. Later, in order to track the reference states well, two sliding mode controllers are introduced based on the linear model and the stability of guidance system is proofed. At last, CAV-H model is utilized to validate the robustness of proposed guidance." @default.
- W2834329510 created "2018-07-19" @default.
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- W2834329510 date "2018-06-01" @default.
- W2834329510 modified "2023-09-24" @default.
- W2834329510 title "A new sliding mode tracking guidance based on three-dimensional trajectory" @default.
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- W2834329510 doi "https://doi.org/10.1109/ccdc.2018.8407431" @default.
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