A model for an airplanes pitch loop is shown in Figure P6.12. Find the range of gain,
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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?
Transcribed Image Text:
Controller Aircraft dynamics Commanded pitch angle K(s + 1) s+ 10 Pitch angle (s+ 4.85) 2 +0.6s + 9 Gyro FIGURE P6.12 Aircraft pitch loop model
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