Control Systems MCQs (Set-4)

As aircraft speed varies, which strategy adjusts controller parameters?

AIntegral reset
BGain scheduling
CPole cancellation
DOutput scaling

Integral windup occurs under what condition?

AIntegrator accumulates during saturation
BDerivative gain becomes zero
CSensor feedback is unity
DPlant poles move left

Which anti-windup method feeds actuator mismatch back to the integrator?

ABack-calculation
BPole cancellation
CDead-zone control
DLead compensation

Which limitation commonly affects ideal derivative action?

ARemoves all steady-state error
BAmplifies high-frequency noise
CReduces sensor bandwidth
DEliminates actuator saturation

PID derivative kick can follow which event?

AConstant plant output
BSlow sensor drift
CStep change in setpoint
DZero proportional gain

Why is practical derivative action filtered?

AIncrease integral windup
BMove every pole to zero
CLimit high-frequency noise gain
DRemove reference tracking

In frequency response, a pure delay adds which phase effect?

AConstant gain increase
BFrequency-dependent phase lag
CPositive phase at all frequencies
DA zero-frequency pole

How much can loop gain increase before instability?

AOutput rise before overshoot
BSensor error at steady state
CGain increase before instability
DTime to reach the setpoint

What does phase margin quantify?

AExtra phase lag before instability
BOutput amplitude at resonance
CController integral time
DPlant input disturbance size

Which angle condition must root-locus points satisfy?

AEven multiple of 90 degrees
BZero degrees at every pole
COdd multiple of 180 degrees
DExactly 45 degrees always

At a root-locus point, what must open-loop magnitude equal?

AClosed-loop magnitude equals zero
BFeedback magnitude equals gain
CPlant phase equals zero
DMagnitude equals reciprocal gain

What internal behavior can unstable pole-zero cancellation conceal?

AA guaranteed stable response
BHidden unstable mode
CZero sensor noise
DInfinite phase margin

In a Routh array, what does a complete zero row indicate?

ANo closed-loop poles
BAll roots at zero
CSymmetric roots about origin
DOnly stable real roots

For the final-value theorem, where must poles of sY(s) lie?

ALeft half-plane
BFinite final value always
CEvery pole is at origin
DOnly for sinusoidal inputs

Discrete-time poles must lie where for asymptotic stability?

AOutside unit circle
BOn positive real axis
CAnywhere in left half-plane
DInside unit circle

Nyquist encirclements of −1 are interpreted using which pole count?

AOpen-loop unstable poles
BReference signal zeros
CSensor bandwidth peaks
DPlant time constants

Laplace-domain representation of a pure delay T is what?

As plus T
BOne over sT
CT times s squared
De^(−sT)

Each additional first-order pole adds which high-frequency magnitude-slope change?

APlus 20 dB per decade
BMinus 20 dB per decade
CMinus 3 dB per decade
DPlus 90 dB per decade

Far above a first-order pole’s corner frequency, its phase approaches what?

APlus 90 degrees
BMinus 90 degrees
CMinus 180 degrees
DZero degrees

Aliasing may result when what sampling condition occurs?

AExcessive damping
BHigh loop gain only
CLow actuator torque
DSampling too slowly

Lead compensation places which element at the lower break frequency?

APole closer to origin
BBoth at origin
CZero closer to origin
DZero at infinity only

Which element lies closer to the origin in a lag compensator?

AZero closer to origin
BBoth at infinity
CPole on imaginary axis
DPole closer to origin

Two-degree-of-freedom control separates which objectives?

AReference tracking and disturbance rejection
BRise time and pole count
CSensor gain and actuator size
DSampling and quantization only

Setpoint weighting can reduce which transient after a command change?

ASteady-state disturbances always
BSensor noise to zero
CPlant model order
DOvershoot after command changes

Physical actuator saturation means the control signal does what?

AControl effort hits a limit
BTransfer function loses poles
CSensor becomes open loop
DReference input turns into noise