E2 16 The position control system for a spacecraft platform is governed by the following equations dp(t) dp(t) dr 2 4p(t) 0 dt v(t) r(t)p(t)

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E2 16 The position control system for a spacecraft platform is governed by the following equations  dp(t) dp(t) dr  2    4p(t)   0 dt v(t) r(t)p(t)

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