Aas 03-100 Integrated Orbit and Attitude Control for a Nanosatellite with Power Constraints

@inproceedings{Naasz2003Aas0I,
  title={Aas 03-100 Integrated Orbit and Attitude Control for a Nanosatellite with Power Constraints},
  author={Bo J. Naasz and Matthew M. Berry and Hye-Young Kim},
  year={2003}
}
Small satellites tend to be power-limited, so that actuators used to control the orbit and attitude must compete with each other as well as with other subsystems for limited electrical power. The Virginia Tech nanosatellite project, HokieSat, must use its limited power resources to operate pulsed-plasma thrusters for orbit control and magnetic torque coils… CONTINUE READING