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- W2701748688 abstract "The attitude control of a spacecraft with a moderate lift/drag ratio during an aeroassisted orbit transfer is considered. The system is non linear, and can be transformed in a linear time-varying one in function of the aerodynamic velocity of the vehicle and the atmospheric density, the purpose of this work is to use adaptive techniques to control the attitude of the vehicle, so that the closed-loop system is time-invariant. The methods proposed here are the Gain-Scheduling technique and the Self-Tuning-Regulator one" @default.
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- W2701748688 date "1993-07-01" @default.
- W2701748688 modified "2023-09-25" @default.
- W2701748688 title "Adaptive Control of an Aerospace Vehicle during an Aeroassisted Orbit Transfer" @default.
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- W2701748688 doi "https://doi.org/10.1016/s1474-6670(17)48856-2" @default.
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