| 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 |