Spacecraft attitude dynamics and control in the presence of large magnetic residuals

2008 ◽  
Vol 41 (2) ◽  
pp. 14054-14059
Author(s):  
Matteo Corno ◽  
Marco Lovera
2013 ◽  
Vol 380-384 ◽  
pp. 298-301
Author(s):  
Xu Min Song ◽  
Yong Chen

The large attitude maneuver is studied in this paper. The quarternion form attitude is appilied to avoid the singularity of dynamic equations, and sliding mode control law based on quarternion is desined. The spacecraft attitude dynamics and control model is builted using simulink, which was valided by simulation.


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