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- W156949927 abstract "Abstract In this paper a new method of satellite attitude control using a bias-momentum called the digital logic coordination control method is described. The key point of method is that the roll-yaw motion state is represented by 8 characteristic codes. codes being processed, the control commands for roll-yaw loop can be generated. The control commands perform the coordination control between precession control and nutation damping. In nutation damping, the absolute value of the attitude error will not increase, but in precession control, the nutation is damped gradually. The controller consists of a number of triggers and gates, so it is simple and reliable. A digital simulation for the attitude control system of a sunpointing satellite has been performed. The result of simulation demonstrates the performance of the new control method." @default.
- W156949927 created "2016-06-24" @default.
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- W156949927 date "1983-07-01" @default.
- W156949927 modified "2023-09-25" @default.
- W156949927 title "A New Method of Satellite Attitude Control using a Bias-Momentum" @default.
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- W156949927 doi "https://doi.org/10.1016/s1474-6670(17)62207-9" @default.
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