Design of Attitude Control Systems for CubeSat-Class Nanosatellite

<table class="table-group" id="tab3"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td align="left">Name</td><td align="center">Values</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td align="left"> Proportional parameters</td><td align="center">0.03</td></tr><tr><td align="left"> Integral parameters</td><td align="center">0.0001</td></tr><tr><td align="left"> Derivative parameters</td><td align="center">0.11</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

PID controller parameters for air bearing testing.

Journal of Control Science and Engineering

tab3

Table 3

Table 3: Design of Attitude Control Systems for CubeSat-Class Nanosatellite 