- = Suppose the relationship between the roll angle o and the ailerons da can be described by the following transfer fun

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Suppose The Relationship Between The Roll Angle O And The Ailerons Da Can Be Described By The Following Transfer Fun 1 (233.58 KiB) Viewed 16 times

- = Suppose the relationship between the roll angle o and the ailerons da can be described by the following transfer function: º(s) a2 da(s) s(s + a1) where ay = 15, az = 3. The maximum aileron deflection is omax = 45°, and the maximum allowed rolling angle is emax = 30°. 3.1. What is the largest possible control error of the roll angle during the flight? (1 mark) 3.2. What type of PID controller should be designed so that the closed-loop system behaves like a second-order system? (1 mark) 3.3. If the closed-loop system is expected to have the damping ratio of 2, what are the parameters of the PID controller? (2 marks) 3.4. What is the type of the closed-loop system, and what is the DC gain? (2 marks)