a. Linear systems do not satisfy superposition. ![]() |
||
b. Linear systems do not satisfy homogeneity. ![]() |
||
c. Linear systems have one equilibrium point at origin. ![]() |
||
d. Linear systems have many equilibrium points at origin. ![]() |
a. Increases, decreases ![]() |
||
b. Increases, increases ![]() |
||
c. Increases, remains unchanged ![]() |
||
d. reRmains unchanged, increases ![]() |
a. “t” ![]() |
||
b. “s” ![]() |
||
c. “d” ![]() |
||
d. “g” ![]() |
a. 0 to 5 ![]() |
||
b. 0 to 1 ![]() |
||
c. 1 to 10 ![]() |
||
d. 0 to 0.1 ![]() |
a. Numerator ![]() |
||
b. Denominator ![]() |
||
c. Natural frequency ![]() |
||
d. Gain ![]() |
a. Flow ![]() |
||
b. Pressure ![]() |
||
c. Current ![]() |
||
d. Torque ![]() |
a. How much the system oscillates ![]() |
||
b. How fast the system oscillates ![]() |
||
c. Size of steady state response ![]() |
||
d. None of the above ![]() |
a. One ![]() |
||
b. Two ![]() |
||
c. Three ![]() |
||
d. Four ![]() |
a. Two ![]() |
||
b. Three ![]() |
||
c. Four ![]() |
||
d. Five ![]() |
a. How much the system oscillates ![]() |
||
b. How fast the system oscillates ![]() |
||
c. Size of steady state response ![]() |
||
d. None of the above ![]() |
a. Natural frequency ![]() |
||
b. Overshoot ![]() |
||
c. Gain ![]() |
||
d. All of the above ![]() |
a. Natural frequency ![]() |
||
b. Damping ratio ![]() |
||
c. Gain ![]() |
||
d. None of the above ![]() |
a. How much the system oscillates ![]() |
||
b. How fast the system oscillates ![]() |
||
c. Size of steady state response ![]() |
||
d. None of the above ![]() |
a. A transfer function is ratio of transform of input to transform of output. ![]() |
||
b. A transfer function is ratio of transform of output to transform of input. ![]() |
||
c. Both A and B ![]() |
||
d. None of the above ![]() |
a. Impulse ![]() |
||
b. Step ![]() |
||
c. Both A and B ![]() |
||
d. None of the above ![]() |
a. Capacitor ![]() |
||
b. Inductor ![]() |
||
c. Resistor ![]() |
||
d. All of the above ![]() |
a. Overdamped ![]() |
||
b. Underdamped ![]() |
||
c. Undamped ![]() |
||
d. All of the above ![]() |
a. Oscillations ![]() |
||
b. Overshoot ![]() |
||
c. Both A and B ![]() |
||
d. None of the above ![]() |
a. Ramp input ![]() |
||
b. Step input ![]() |
||
c. Constant input ![]() |
||
d. None of the above ![]() |
a. Gear train ![]() |
||
b. Four-bar linkage ![]() |
||
c. Transformer ![]() |
||
d. All of the above ![]() |
a. Transfer function applies to nonlinear system. ![]() |
||
b. Transfer function applies to stationary systems. ![]() |
||
c. During transfer function, computation all initial conditions are assumed as zero. ![]() |
||
d. Transfer function describes input-output dynamics. ![]() |
a. Loop method ![]() |
||
b. Node method ![]() |
||
c. Complex impedances ![]() |
||
d. Perimeter method ![]() |
a. Linear systems satisfy superposition. ![]() |
||
b. Linear systems satisfy homogeneity. ![]() |
||
c. Linear systems have two equilibrium points at origin. ![]() |
||
d. Linear systems have one equilibrium point at origin. ![]() |
a. Input variables originate outside the system. ![]() |
||
b. Input variables originate inside the system. ![]() |
||
c. Input variables are not affected by what happens in a system. ![]() |
||
d. All of the above ![]() |
a. Output variables are not influenced by input variables. ![]() |
||
b. Output variables do not regulate the system. ![]() |
||
c. Output variables do not monitor the system. ![]() |
||
d. Output variables are influenced by input variables. ![]() |
a. Two ![]() |
||
b. Three ![]() |
||
c. Four ![]() |
||
d. Five ![]() |
a. Time ![]() |
||
b. Frequency ![]() |
||
c. Both A and B ![]() |
||
d. None of the above ![]() |
a. Power gain ![]() |
||
b. Phase ![]() |
||
c. Margin ![]() |
||
d. Percentage overshoot ![]() |
a. 0 ![]() |
||
b. 1 ![]() |
||
c. -1 ![]() |
||
d. 2 ![]() |
a. 2 ![]() |
||
b. 4 ![]() |
||
c. 8 ![]() |
||
d. 10 ![]() |
a. 2 ![]() |
||
b. 4 ![]() |
||
c. 8 ![]() |
||
d. 10 ![]() |
a. 0 ![]() |
||
b. 180 ![]() |
||
c. 360 ![]() |
||
d. -180 ![]() |
a. Decibels ![]() |
||
b. Logarithmic scale ![]() |
||
c. Degrees ![]() |
||
d. Percentage overshoot ![]() |
a. Decibels ![]() |
||
b. Logarithmic scale ![]() |
||
c. Degrees ![]() |
||
d. Percentage overshoot ![]() |
a. Decibels ![]() |
||
b. Logarithmic scale ![]() |
||
c. Degrees ![]() |
||
d. Percentage overshoot ![]() |
a. More ![]() |
||
b. Less ![]() |
||
c. The same ![]() |
||
d. Zero ![]() |
a. Increases, decreases ![]() |
||
b. Increases, increases ![]() |
||
c. Increases, remains unchanged ![]() |
||
d. Remains unchanged, increases ![]() |
a. First ![]() |
||
b. Second ![]() |
||
c. Third ![]() |
||
d. Fourth ![]() |
a. 6 percent ![]() |
||
b. 8 percent ![]() |
||
c. 10 percent ![]() |
||
d. 12 percent ![]() |
a. 1 percent ![]() |
||
b. 0.05 percent ![]() |
||
c. 10 percent ![]() |
||
d. 0 percent ![]() |
a. 0 ![]() |
||
b. 1 ![]() |
||
c. 2 ![]() |
||
d. 3 ![]() |
a. 0 ![]() |
||
b. 1 ![]() |
||
c. 2 ![]() |
||
d. 3 ![]() |
a. Frequency of oscillations ![]() |
||
b. Reciprocal of time constant ![]() |
||
c. Undamped natural frequency ![]() |
||
d. None of the above ![]() |
a. Frequency of oscillations ![]() |
||
b. Reciprocal of time constant ![]() |
||
c. Undamped natural frequency ![]() |
||
d. None of the above ![]() |
a. Frequency of oscillations ![]() |
||
b. Reciprocal of time constant ![]() |
||
c. Undamped natural frequency ![]() |
||
d. None of the above ![]() |
a. Impulse ![]() |
||
b. Step ![]() |
||
c. Ramp ![]() |
||
d. Random ![]() |
a. At open loop zeros ![]() |
||
b. At closed loop zeros ![]() |
||
c. At open loop poles ![]() |
||
d. At closed loop poles ![]() |
a. At open loop zeros ![]() |
||
b. At closed loop zeros ![]() |
||
c. At open loop poles ![]() |
||
d. At closed loop poles ![]() |
a. A Nyquist plot uses the same plot to display amplitude and phase. ![]() |
||
b. A Nyquist plot cannot depict if a system is stable or unstable. ![]() |
||
c. Both A and B ![]() |
||
d. None of the above ![]() |
a. Phase margin ![]() |
||
b. Gain margin ![]() |
||
c. Both A and B ![]() |
||
d. None of the above ![]() |
a. Difference between input and measured varying output ![]() |
||
b. Difference between input and measured constant output ![]() |
||
c. Difference between measured constant input and measured varying output ![]() |
||
d. None of the above ![]() |
a. 0.2 ![]() |
||
b. 0.4 ![]() |
||
c. 0.6 ![]() |
||
d. 0.8 ![]() |
a. Phase lead ![]() |
||
b. Phase lag ![]() |
||
c. Integration ![]() |
||
d. All of the above ![]() |
a. Phase lead ![]() |
||
b. Phase lag ![]() |
||
c. Integration ![]() |
||
d. All of the above ![]() |
a. Open-loop time response ![]() |
||
b. Closed-loop time response ![]() |
||
c. Open-loop frequency response ![]() |
||
d. Closed-loop frequency response ![]() |
a. 0.1 ![]() |
||
b. 1 ![]() |
||
c. 2 ![]() |
||
d. 0 ![]() |
a. Added to ![]() |
||
b. Subtracted from ![]() |
||
c. Multiplied with ![]() |
||
d. Divided by ![]() |
a. 1 ![]() |
||
b. 0.1 ![]() |
||
c. 2 ![]() |
||
d. 0.01 ![]() |
a. P ![]() |
||
b. D ![]() |
||
c. PD ![]() |
||
d. PID ![]() |
a. Zero ![]() |
||
b. One ![]() |
||
c. Infinity ![]() |
||
d. Ten ![]() |
a. Zero ![]() |
||
b. One ![]() |
||
c. Infinity ![]() |
||
d. Ten ![]() |
a. AC ![]() |
||
b. DC ![]() |
||
c. On-Off ![]() |
||
d. Integral ![]() |
a. Phase margin ![]() |
||
b. Gain margin ![]() |
||
c. Natural frequency ![]() |
||
d. Overshoot ![]() |
a. 0.1 ![]() |
||
b. 0.01 ![]() |
||
c. 0 ![]() |
||
d. 1 ![]() |
a. Sensor ![]() |
||
b. Input ![]() |
||
c. Plant ![]() |
||
d. None of the above ![]() |
a. Sensor ![]() |
||
b. Input ![]() |
||
c. Plant ![]() |
||
d. None of the above ![]() |
a. Input ![]() |
||
b. Output ![]() |
||
c. Control effort ![]() |
||
d. Response ![]() |
a. Input ![]() |
||
b. Measured input ![]() |
||
c. Output ![]() |
||
d. Error ![]() |
a. Proportional control ![]() |
||
b. Integral control ![]() |
||
c. On-Off control ![]() |
||
d. Derivative control ![]() |
a. Zeros ![]() |
||
b. Poles ![]() |
||
c. Gain ![]() |
||
d. Phase ![]() |
a. Steady state error ![]() |
||
b. Phase margin ![]() |
||
c. Open loop gain ![]() |
||
d. Closed loop gain ![]() |
a. Proportional ![]() |
||
b. Integral ![]() |
||
c. On-Off ![]() |
||
d. Derivative ![]() |
a. Overshoot is within plus and minus 1 percent. ![]() |
||
b. Overshoot is within plus and minus 2 percent. ![]() |
||
c. Overshoot is within plus and minus 3 percent. ![]() |
||
d. Overshoot is within plus and minus 4 percent. ![]() |
a. Response is fast. ![]() |
||
b. There is a short rise time. ![]() |
||
c. There is a short settling time. ![]() |
||
d. All of the above ![]() |
a. Maintain gain ![]() |
||
b. Increase gain ![]() |
||
c. Decrease gain ![]() |
||
d. None of the above ![]() |
a. Increase phase margin ![]() |
||
b. Decrease gain ![]() |
||
c. Maintain phase margin ![]() |
||
d. None of the above ![]() |
a. Bandwidth increases ![]() |
||
b. Bandwidth decreases ![]() |
||
c. Bandwidth is constant ![]() |
||
d. None of the above ![]() |
a. Input ![]() |
||
b. System ![]() |
||
c. Output ![]() |
||
d. All of the above ![]() |
a. “poly” ![]() |
||
b. “csim” ![]() |
||
c. “step” ![]() |
||
d. “evans” ![]() |
a. “ss2tf” ![]() |
||
b. “tf2ss” ![]() |
||
c. “roots” ![]() |
||
d. “evans” ![]() |
a. “syslin” ![]() |
||
b. “csim” ![]() |
||
c. “step” ![]() |
||
d. “evans” ![]() |
a. “syslin” ![]() |
||
b. “csim” ![]() |
||
c. “step” ![]() |
||
d. “evans” ![]() |
a. “syslin” ![]() |
||
b. “csim” ![]() |
||
c. “roots” ![]() |
||
d. “evans” ![]() |
a. “syslin” ![]() |
||
b. “csim” ![]() |
||
c. “roots” ![]() |
||
d. “evans” ![]() |
a. “roots” ![]() |
||
b. “csim” ![]() |
||
c. “syslin” ![]() |
||
d. “evans” ![]() |
a. “syslin” ![]() |
||
b. “csim” ![]() |
||
c. “roots” ![]() |
||
d. “evans” ![]() |
a. “syslin” ![]() |
||
b. “csim” ![]() |
||
c. “roots” ![]() |
||
d. “evans” ![]() |
a. “syslin” ![]() |
||
b. “csim” ![]() |
||
c. “roots” ![]() |
||
d. “evans” ![]() |
a. “ss2tf” ![]() |
||
b. “horner” ![]() |
||
c. “roots” ![]() |
||
d. “evans” ![]() |
a. “csim” ![]() |
||
b. “step” ![]() |
||
c. “bode” ![]() |
||
d. “nyquist” ![]() |
a. “csim” ![]() |
||
b. “step” ![]() |
||
c. “bode” ![]() |
||
d. “nyquist” ![]() |
a. “syslin” ![]() |
||
b. “csim” ![]() |
||
c. “step” ![]() |
||
d. “evans” ![]() |
a. “csim” ![]() |
||
b. “step” ![]() |
||
c. “bode” ![]() |
||
d. “nyquist” ![]() |
a. “syslin” ![]() |
||
b. “csim” ![]() |
||
c. “step” ![]() |
||
d. “evans” ![]() |
a. Vacuum tubes ![]() |
||
b. Transformers ![]() |
||
c. Microprocessors ![]() |
||
d. Opamps ![]() |
a. P controller ![]() |
||
b. PD controller ![]() |
||
c. PI controller ![]() |
||
d. PID controller ![]() |
a. P controller ![]() |
||
b. PD controller ![]() |
||
c. PI controller ![]() |
||
d. PID controller ![]() |
a. Digital control system uses digital computers. ![]() |
||
b. Digital control system uses digital signals. ![]() |
||
c. Measured data is converted from analog to digital. ![]() |
||
d. Measured data is converted from digital to analog. ![]() |
a. Manipulation is done in digital form. ![]() |
||
b. Manipulation is done in analog form. ![]() |
||
c. Both A and B ![]() |
||
d. None of the above ![]() |
a. Many systems are analog. ![]() |
||
b. Many systems are digital. ![]() |
||
c. Both A and B ![]() |
||
d. None of the above ![]() |
a. Performance of analog is greater than performance of digital. ![]() |
||
b. Performance of analog is less than performance of digital. ![]() |
||
c. Performance of analog is equal to performance of digital. ![]() |
||
d. None of the above ![]() |
a. Performance of analog is greater than performance of digital. ![]() |
||
b. Performance of analog is less than performance of digital. ![]() |
||
c. Performance of analog is equal to performance of digital. ![]() |
||
d. None of the above. ![]() |
a. Laplace ![]() |
||
b. State-space ![]() |
||
c. Both A and B ![]() |
||
d. None of the above ![]() |
a. Robust control systems have high sensitivities. ![]() |
||
b. Robust control systems have low sensitivities. ![]() |
||
c. Robust control is stable over wide range of parameter variations. ![]() |
||
d. All of the above ![]() |