This paper discusses the design arid validation of the space magnetic field
simulator at the University of Naples. The simulator is designed to reprod
uce, with a predetermined uniformity, the magnetic field vector as sensed b
y an orbiting satellite in an assigned volume about the simulator's geometr
ical center. The simulator will be used primarily for ground testing the ma
gnetic attitude control subsystem onboard the university microsatellite SMA
RT. The paper describes the criteria as well as the mathematical model used
for the simulator design. The design aims mainly at developing a simulator
configuration that maximizes the volume in which the desired magnetic fiel
d vector is realized with a predetermined uniformity with respect to a nomi
nal field. The simulator is configured as art open-loop system, in which fi
xed currents are used to nullify the local magnetic field. Precision curren
ts are then added to the fixed ones to accurately reproduce, in the test vo
lume, the in-orbit magnetic field vector variation. Results of the simulato
r validation tests are presented.