An attitude control system for a satellite vehicle within the earth's atmosphere is
Chapter 0, Problem P7.6(choose chapter or problem)
An attitude control system for a satellite vehicle within the earth's atmosphere is shown in Figure P7.6. The transfer functions of the system are G(5) = K(s + 0.20) (5 + 0.90)(5 - 0.60)(5 - 0.10)
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