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- W2672107017 abstract "Abstract This paper treats the atmospheric orbit transfert of a spacecraft. The main problem developed is the atmospheric flight. The guidance law is obtained by using two classical non linear guidance methods: the trajectory tracking, and the sliding mode control technique. A model reduction by singular perturbations is also considered. The point is that the system is required to track a pre-defined reference trajectory, such that the vehicle flies, from given initial conditions, to defined exit conditions. To test the performances of the guidance law, a robustness study is done for the atmosperic density variations" @default.
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- W2672107017 date "1993-07-01" @default.
- W2672107017 modified "2023-10-01" @default.
- W2672107017 title "Online Computable Guidance Methods for the Atmospheric Flight of a Spacecraft" @default.
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- W2672107017 doi "https://doi.org/10.1016/s1474-6670(17)48836-7" @default.
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