Engineering, 13.11.2019 18:31 isaiahromero15
Where the normalized parameters are: • j = 10: spacecraft inertia, n·m·sec2 /rad • θr: reference satellite attitude, rad • θ: actual satellite attitude, rad • hy = 1: sensor scale factor, v/rad • hr = 1: reference sensor scale factor, v/rad • w: disturbance torque, n·m (a) use proportional (p) control and give the range of gain values for which the system is stable.
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Where the normalized parameters are: • j = 10: spacecraft inertia, n·m·sec2 /rad • θr: reference...
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