All Electronics & Telecommunication MCQs
Browse Electronics & Telecommunication Engineering MCQs with four options, hidden answers, concise explanations and references where available. Questions are organized in pages of up to 100 for focused practice.
Question 601
Signals & SystemsSampling
- A2 kHz
- B3 kHz
- C6 kHz
- D9 kHz
Question 602
Signals & SystemsSampling
- ARectangular frequency response
- BTriangular time response only
- CConstant impulse at every sample
- DHigh-pass response
Question 603
Signals & SystemsDTFT
- Aπ
- B2π
- C4π
- DIt is not periodic
Question 604
Signals & SystemsDTFT
- A0
- B1
- Ce^(-jω)
- D2πdelta(ω) only
Question 605
Signals & SystemsDTFT
- Ae^(-jωn0)
- Be^(jωn0)
- Cn0
- Djω
Question 606
Signals & SystemsDTFT
- AX(e^(-jω))=X*(e^(jω))
- BX(e^(-jω))=-X*(e^(jω)) always
- CX(e^(jω))=0
- DX(e^(jω)) is always purely real
Question 607
Signals & SystemsLTI Frequency Response
- AThe same frequency
- BTwice the input frequency
- CZero frequency only
- DA random frequency
Question 608
Signals & SystemsSystem Response
- A(1-e^(-5t))u(t)
- B5e^(-5t)u(t)
- Ce^(-t)u(t)
- D5u(t)
Question 609
Control SystemsControl Fundamentals
- AOpen-loop system
- BClosed-loop system
- CAdaptive system only
- DNonlinear feedback system
Question 610
Control SystemsControl Fundamentals
- AOpen-loop system
- BClosed-loop system
- CUncontrolled system
- DIsolated system
Question 611
Control SystemsFeedback
- AReduced sensitivity to parameter variations
- BInfinite output for every input
- CElimination of all components
- DGuaranteed zero error for every system
Question 612
Control SystemsFeedback
- AReference minus feedback signal
- BReference plus feedback signal always
- COutput multiplied by input
- DFeedback divided by reference
Question 613
Control SystemsTransfer Functions
- AG(s)/(1+G(s)H(s))
- BG(s)/(1-G(s)H(s))
- CH(s)/(1+G(s))
- DG(s)H(s) only
Question 614
Control SystemsFeedback
Question 615
Control SystemsTransfer Functions
- ALaplace transform of output divided by Laplace transform of input
- BInput divided by output
- COutput plus input
- DDerivative of output only
Question 616
Control SystemsTransfer Functions
- ANumerator zero
- BDenominator zero
- CGain always unity
- DInput zero
Question 617
Control SystemsTransfer Functions
Question 618
Control SystemsTransfer Functions
Question 619
Control SystemsTime Response
- ATime constant
- BDamping ratio
- CNatural frequency
- DSteady-state gain only
Question 620
Control SystemsTime Response
Question 621
Control SystemsTime Response
Question 622
Control SystemsSecond-Order Systems
- As²+2ζωn s+ωn²
- Bs²+ζs+ωn
- Cs+ωn²
- Ds²+2ωn
Question 623
Control SystemsSecond-Order Systems
- ADamping ratio
- BNatural frequency
- CStatic gain
- DTime delay
Question 624
Control SystemsSecond-Order Systems
- AUndamped natural frequency
- BDamping ratio
- CDC error
- DFeedback factor
Question 625
Control SystemsSecond-Order Systems
- AUnderdamped
- BCritically damped
- COverdamped
- DUndamped only
Question 626
Control SystemsSecond-Order Systems
- AUnderdamped
- BCritically damped
- COverdamped
- DUnstable necessarily
Question 627
Control SystemsSecond-Order Systems
- AUnderdamped
- BUndamped
- COverdamped
- DCritically damped
Question 628
Control SystemsSecond-Order Systems
- AUndamped
- BCritically damped
- COverdamped
- DFirst order
Question 629
Control SystemsSecond-Order Systems
- A3 rad/s
- B5 rad/s
- C6 rad/s
- D25 rad/s
Question 630
Control SystemsSecond-Order Systems
Question 631
Control SystemsTime Response
- AIncrease
- BDecrease
- CRemain exactly unchanged
- DBecome infinite
Question 632
Control SystemsSteady-State Error
- AZero only
- BInfinity
- COne second always
- DThe natural period only
Question 633
Control SystemsSystem Type & Error Constants
- AZeros at the origin
- BOpen-loop poles at the origin
- CClosed-loop poles in the right half-plane
- DFinite zeros only
Question 634
Control SystemsSteady-State Error
- AZero
- BFinite and nonzero
- CInfinite in every case
- DAlways -1
Question 635
Control SystemsSteady-State Error
- AZero
- BFinite nonzero
- CInfinite
- DEqual to Kv
Question 636
Control SystemsSteady-State Error
- A1/Kp
- B1/Kv
- C1/Ka
- DAlways zero
Question 637
Control SystemsSteady-State Error
- AZero
- B1/Kv
- C1/Ka
- DInfinite
Question 638
Control SystemsStatic Error Constants
- Alim s->0 G(s)
- Blim s->0 sG(s)
- Clim s->0 s²G(s)
- Dlim s->infinity G(s)
Question 639
Control SystemsStatic Error Constants
- Alim s->0 G(s)
- Blim s->0 sG(s)
- Clim s->0 s²G(s)
- Dlim s->infinity sG(s)
Question 640
Control SystemsStatic Error Constants
- Alim s->0 G(s)
- Blim s->0 sG(s)
- Clim s->0 s²G(s)
- Dlim s->infinity s²G(s)
Question 641
Control SystemsSteady-State Error
Question 642
Control SystemsSteady-State Error
Question 643
Control SystemsSteady-State Error
Question 644
Control SystemsSteady-State Error
Question 645
Control SystemsRouth-Hurwitz
- AAbsolute stability without explicitly calculating all roots
- BOnly steady-state gain
- COnly system bandwidth
- DInput signal amplitude
Question 646
Control SystemsRouth-Hurwitz
- AAlways sufficient for stability
- BNecessary but not generally sufficient for Hurwitz stability
- CNever relevant
- DSufficient only for every fourth-order system
Question 647
Control SystemsRouth-Hurwitz
- ALeft half-plane
- BRight half-plane
- COrigin only
- DImaginary axis only
Question 648
Control SystemsRouth-Hurwitz
- AAll positive
- BAll negative
- CAlternating in sign
- DZero
Question 649
Control SystemsRouth-Hurwitz
- AK>6
- B0<K<6
- CK<0 only
- DK=6 only
Question 650
Control SystemsRouth-Hurwitz
- AStability boundary
- BAlways strictly stable
- CAlways overdamped
- DOrigin with three repeated poles
Question 651
Control SystemsRoot Locus
- ALoop gain K
- BInput amplitude only
- CTime variable t
- DOutput voltage only
Question 652
Control SystemsRoot Locus
- AOpen-loop poles
- BOpen-loop zeros
- CClosed-loop zeros only
- DImaginary-axis crossings
Question 653
Control SystemsRoot Locus
- AOpen-loop zeros, including zeros at infinity
- BOpen-loop poles only
- CThe origin only
- DThe positive real axis only
Question 654
Control SystemsRoot Locus
- AOpen-loop poles
- BOpen-loop finite zeros only
- CClosed-loop zeros
- DBreakaway points
Question 655
Control SystemsRoot Locus
Question 656
Control SystemsBlock Diagram Reduction
- AG1+G2
- BG1G2
- CG1/G2 always
- DG1-G2
Question 657
Control SystemsBlock Diagram Reduction
- AG1G2
- BG1+G2
- CG1/G2
- D1/(G1+G2)
Question 658
Control SystemsRoot Locus
- A(2q+1)180°/(n-m)
- B2q×180°/(n+m)
- Cq×90°/n
- D180°/(n+m) only
Question 659
Control SystemsRoot Locus
- A(sum of poles - sum of zeros)/(n-m)
- B(sum of poles + sum of zeros)/(n+m)
- CProduct of poles divided by product of zeros
- DOrigin in every system
Question 660
Control SystemsRoot Locus
Question 661
Control SystemsRoot Locus
- A0°, 120°, 240°
- B60°, 180°, 300°
- C90°, 180°, 270°
- D45°, 180°, 315°
Question 662
Control SystemsRoot Locus
- AEven
- BOdd
- CZero only
- DAlways two
Question 663
Control SystemsRoot Locus
- AdK/ds=0
- BK=0 only
- Cd²K/ds²=0 only
- Ds=0 always
Question 664
Control SystemsBode Plot
- ADecibels
- BRadians
- CSeconds
- DOhms
Question 665
Control SystemsBode Plot
- A10 dB
- B20 dB
- C40 dB
- D100 dB
Question 666
Control SystemsBode Plot
- A-20 dB
- B-10 dB
- C0 dB
- D20 dB
Question 667
Control SystemsBode Plot
- A+20 dB/decade
- B-20 dB/decade
- C-40 dB/decade
- D0 dB/decade
Question 668
Control SystemsBode Plot
- A+20 dB/decade
- B-20 dB/decade
- C+40 dB/decade
- D0 dB/decade
Question 669
Control SystemsBode Plot
Question 670
Control SystemsBode Plot
- A-90°
- B-45°
- C+45°
- D+90° exactly at all frequencies
Question 671
Control SystemsStability Margins
- A0 dB
- B-180 dB
- C1 dB
- DInfinite
Question 672
Control SystemsStability Margins
- A0°
- B+90°
- C-90°
- D-180° modulo 360°
Question 673
Control SystemsStability Margins
- AGain crossover frequency
- BPhase crossover frequency only
- CNatural frequency always
- DDC frequency only
Question 674
Control SystemsStability Margins
- AGain crossover frequency
- BPhase crossover frequency
- CResonant frequency only
- DSampling frequency
Question 675
Control SystemsStability Margins
Question 676
Control SystemsStability Margins
Question 677
Control SystemsStability Margins
- A3.01 dB
- B6.02 dB
- C10 dB
- D20 dB
Question 678
Control SystemsNyquist Stability
Question 679
Control SystemsNyquist Stability
- ANo encirclement of -1+j0
- BOne clockwise encirclement of -1+j0
- COne counterclockwise encirclement always
- DAn encirclement of the origin
Question 680
Control SystemsNyquist Stability
- As-plane through the loop transfer function
- BTime domain directly into the z-plane only
- COutput plane into the input plane
- DRoot locus into the Routh array
Question 681
Control SystemsFrequency Response
- AGreater relative stability and damping tendency
- BGuaranteed instability
- CZero bandwidth
- DInfinite steady-state error
Question 682
Control SystemsBode Plot
- A1 rad/s
- B10 rad/s
- C100 rad/s
- D1000 rad/s
Question 683
Control SystemsTime Response
- Aπ/ωn
- Bπ/[ωn√(1-ζ²)]
- C4/(ζωn)
- D1/(ζωn)
Question 684
Control SystemsTime Response
- A2 rad/s
- B3 rad/s
- C4 rad/s
- D5 rad/s
Question 685
Control SystemsTime Response
- A0.314 s
- B0.628 s
- C0.785 s
- D1.571 s
Question 686
Control SystemsTime Response
- A1/(ζωn)
- B2/(ζωn)
- C4/(ζωn)
- Dπ/(ζωn)
Question 687
Control SystemsTime Response
- A0.2 s
- B0.4 s
- C0.8 s
- D2 s
Question 688
Control SystemsTime Response
- A100e^[-πζ/√(1-ζ²)]
- B100ζωn
- C100/(1+ζ)
- D100e^(-ωn)
Question 689
Control SystemsTime Response
Question 690
Control SystemsControllers
- Au(t)=Kp e(t)
- Bu(t)=Ki∫e(t)dt only
- Cu(t)=Kd de(t)/dt only
- Du(t)=0
Question 691
Control SystemsControllers
- ASteady-state error for suitable stable systems
- BAll measurement noise
- CPlant order
- DEvery transient oscillation
Question 692
Control SystemsControllers
- AThe rate of change of error
- BOnly accumulated error
- COnly constant error magnitude
- DThe reference amplitude squared
Question 693
Control SystemsControllers
- AKp+Ki/s+Kd s
- BKp s+Ki+Kd/s²
- CKp/(s+1) only
- DKi s only
Question 694
Control SystemsControllers
- A0
- B1
- C2
- DIt always decreases type
Question 695
Control SystemsCompensators
- APhase margin and transient response
- BSteady-state error only with no transient effect
- CSensor noise generation
- DSystem type by two automatically
Question 696
Control SystemsCompensators
- ASteady-state accuracy by increasing low-frequency gain
- BHigh-frequency noise amplification
- CNatural frequency to infinity
- DPhase lead at all frequencies
Question 697
Control SystemsCompensators
- ACloser to the origin than its pole on the negative real axis
- BFarther from the origin than its pole
- CAt exactly the same location as its pole
- DIn the right half-plane necessarily
Question 698
Control SystemsState Space
- Ax_dot=Ax+Bu, y=Cx+Du
- By=G(s)x only
- Cx=Ay²
- Du=Cy only
Question 699
Control SystemsState Space
- AMinimal dynamic model
- BInput amplitude
- CSteady-state error constant
- DFeedback sensor gain only
Question 700
Control SystemsState Space
- APoles for a minimal state-space realization
- BZeros only
- CInput frequencies only
- DStatic error constants