Case Study #7: Satellite Reorientation Control

Part of the Understanding Complex Systems book series (UCS)


Chapter 12 presents HSSPFC applied to a slewing spacecraft problem. The specific slewing spacecraft problem is a Multi-Input-Multi-Output (MIMO) three-axis spacecraft that employs Proportional-Integral-Derivative (PID) tracking control with numerical simulation results. This problem provides an interesting complication due to the three-axis rigid body rotation sequence.


Tracking Control Attitude Control System Model Reference Adaptive Control Rigid Body Mode Control Lyapunov Function 
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© Springer-Verlag London Limited 2011

Authors and Affiliations

  1. 1.Sandia National LaboratoriesAlbuquerqueUSA

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