Question: E2.16 The position control system for a spacecraft platform is governed by the following equations: dp(t) +2dp(t) 2- dt2 +4p(t) = 0 dt v(t)=r(t)-p(t)

E2.16 The position control system for a spacecraft platform is governed by the following equations:dp(t) +2dp(t) 2- dt2 +4p(t) = 0 dt v(t)=r(t)-p(t)image text in transcribed

dp(t) +2dp(t) 2- dt2 +4p(t) = 0 dt v(t)=r(t)-p(t)

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