How do I calculate the steady-state pitch angle for the unity step input for the above...

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Electrical Engineering

  

How do I calculate the steady-state pitch angle for the unitystep input for the above system in matlab workspace?

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consider the system with the dynamic equations in the Laplacedomain and the openloop transfer function of the aircraft pitch asgiven below sAs 0213 As 467 Qs 0332 ssQs 00139 As0426Qs 00203 sss 467 QsPs s s 1161s 01784 s3 0738 s2 0821sFor a step reference the design criteria are the followingOvershoot less than 10Rise time less than 2 secondsSettling time less than 10 secondsSteadystate error less than 2From the analysis of open loop response we can see that the openloop response is unstable In order to    See Answer
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