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Aeronautical & Aerospace Engineering : Avionics - Quiz(MCQ)
Integral of a control system provides ____
A)
Low steady state error
B)
infinite gain
C)
Reduced overshoot
D)
Gain proportional to error

Correct Answer :   Low steady state error


Explanation : Integral of error control eliminates steady-state errors and reduces the following lag. The integral of error term increases the loop gain at low frequencies up to theoretically infinite gain at dc so that there are zero steady-state errors due to out of trim external moments or forces acting on the aircraft.

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