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- W120825144 abstract "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." @default.
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- W120825144 date "2011-01-01" @default.
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- W120825144 title "Case Study #7: Satellite Reorientation Control" @default.
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