a)is the aircraft stable about the equilibrium represented by the transfer function?b) Using proportional feedback,what is the range of acceptable gains for the closed loop systen to be stable?c) Design a feedback control system that allows the pilot to command a pitch angle with overshoot less than or equal to 4.15% and a natural frequency of greater than or equal to 0.99 rad/sd) Design a feedback control system that allows the pilot to command a pitch angle with the same overshoot and a natural frequency of one half the system in part c. 2) An aircraft2/8/2e(s)₂ (5)designNc) DesignisS-4s²-0.65 +9• pitch angle (radians)Se elevator deflection (radians)open loop transfer functionstablaa) Is the aircraft "about the equilibrium represent by (3)theofb) using proportional feedback, what isgaindacceptablerangethe closed loop system to be stable?a feedback control system that allows the pilot topitchanglewith overshoot less than oregud!!to10.98 reda4.15% and a noturd frequency of greater than ord) Design a feedback control system that allows the pilot tocommand a pitch angle with the same overshoot and aof the half of system in part c)naturalEvegueray

a)is the aircraft stable about the equilibrium represented by the transfer function? b) Using proportional feedback,what is the range of acceptable gains for the closed loop systen to be stable? c) Design a feedback control system that allows the pilot to command a pitch angle with overshoot less than or equal to 4.15% and a natural frequency of greater than or equal to 0.99 rad/s d) Design a feedback control system that allows the pilot to command a pitch angle with the same overshoot and a natural frequency of one half the system in part c.

a)is the aircraft stable about the equilibrium represented by the transfer function? b) Using proportional feedback,what is the range of acceptable gains for the closed loop systen to be stable? c) Design a feedback control system that allows the pilot to command a pitch angle with overshoot less than or equal to 4.15% and a natural frequency of greater than or equal to 0.99 rad/s d) Design a feedback control system that allows the pilot to command a pitch angle with the same overshoot and a natural frequency of one half the system in part c.

Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)

8th Edition

ISBN:9781305387102

Author:Kreith, Frank; Manglik, Raj M.

Publisher:Kreith, Frank; Manglik, Raj M.

Chapter4: Numerical Analysis Of Heat Conduction

Section: Chapter Questions

Problem 4.6P

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