Operational spacecraft undergo substantial mass

Reference no: EM131127783

Operational spacecraft undergo substantial mass property and configuration changes during their lifetime [25]. For example, the inertias change considerably during operations. Consider the orientation control system shown in Figure AP9.1.

(a) Plot the Bode diagram, and determine the gain and phase margins when ω_n² = 15,267. (b) Repeat part (a) when ω_n²= 9500. Note the effect of changing ω_n²by 38%.

Reference no: EM131127783

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