Research Article

Design and Numerical Validation of an Algorithm for the Detumbling and Angular Rate Determination of a CubeSat Using Only Three-Axis Magnetometer Data

Table 4

Results from some selected test cases for ω = [10 10 10] deg/sec.

i = 0 deg
Altitude (km)700600500400
Detumbling time (sec)9266904686528267
Settling time for (sec)105012361158996
Settling time for (sec)1270125011801191
Settling time for (sec)1218116811531192

i = 30 deg
Altitude (km)700600500400
Detumbling time (sec)9078893285488166
Settling time for (sec)117011691080975
Settling time for (sec)1246124311561055
Settling time for (sec)1239112911651126

i = 60 deg
Altitude (km)700600500400
Detumbling time (sec)8299683259825796
Settling time for (sec)116610881066958
Settling time for (sec)124613341032966
Settling time for (sec)1217117810251094

i = 90 deg
Altitude (km)700600500400
Detumbling time (sec)7964622851704374
Settling time for (sec)1182115311021022
Settling time for (sec)123411731076997
Settling time for (sec)1454154110791012