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MEC3457 / MAE3408 Systems and control/Aerospace control - MUM S2 2025
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Why do we have four transfer functions for this one system instead of one?
Why do underdamped systems show oscillation?
What do the eigenvalues of the system matrix represent?
What does the natural response of this system tell you?
If the dominant pole is negative but a different, much less impactful pole is positive, what does that mean for system stability?
What will be the coefficient vector of the characteristic equation of close loop transfer function : H(s) = 3.1s3 + 2.4s2 +0.9s + 2.6 (6s + 2)(3s + 4)
The following figure shows the block diagram of a SISO feedback control system
K.... is the constant-gain corrector,E(s).... is the error signalG(s).... is the open loop transfer function andH(s) =1 .... is the unity feedback transfer function
Select ALL the options that can be used to compute the CLTF of this system in MATLAB
Do the partial fraction decomposition of the following fraction finding the values for A, B and C: