A model for an airplanes pitch loop is shown in Figure

Chapter 6, Problem 56

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QUESTION:

A model for an airplane’s pitch loop is shown in Figure P6.12. Find the range of gain, K, that will keep the system stable. Can the system ever be unstable for positive values of K?

                             

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QUESTION:

A model for an airplane’s pitch loop is shown in Figure P6.12. Find the range of gain, K, that will keep the system stable. Can the system ever be unstable for positive values of K?

                             

ANSWER:

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According to the model of an airplane pitch loop, as given below,

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