Engineering, 05.05.2020 17:33, juliawatakip5fmg7

A controller for a satellite attitude control with transfer function G = 1 s 2 has been designed with a unity feedback structure and has the transfer function D(s) = 8(s+2) s+4 . Find the system type and the corresponding error constant for this system.

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A controller for a satellite attitude control with transfer function G = 1 s 2 has been designed wit...