To satisfy the requirements for small satellites that seek agile slewing with peak power, this paper investigates integrated power and\nattitude control using variable-speed control moment gyros (VSCMGs) that consider the mass and inertia of gimbals and wheels.\nThe paper also details the process for developing the controller by considering various environments in which the controller may be\nimplemented. A fuzzy adaptive disturbance observer (FADO) is proposed to estimate and compensate for the effects of equivalent\ndisturbances.The algorithms can simultaneously track attitude and power.The simulation results illustrate the effectiveness of the\ncontrol approach, which exhibits an improvement of 80 percent compared with alternate approaches that do not employ a FADO.
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