Q 3. An Indian jet aircraft employs a system for monitoring the RPM, pressure, and temperature values of its engines using sensors that operate as follows: RPM sensor output = 0 only when speed < 4600 rpm P sensor output = 0 only when pressure <210 psi T sensor output = 0 only when temperature < 180°F Figure shows the logic circuit that controls a cockpit warning light for certain combinations of engine conditions. Assume that a HIGH at output W activates the warning light. i. Write Boolean function for W. ii. Determine what engine conditions will give a warning to the pilot. Temp sonsor Prossure Warning light sensor RPM sonsor

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Q 3. An Indian jet aircraft employs a system for monitoring the RPM, pressure, and
temperature values of its engines using sensors that operate as follows:
RPM sensor output = 0 only when speed < 4600 rpm
P sensor output = 0 only when pressure < 210 psi
T sensor output = (0 only when temperature < 180°F
Figure shows the logic circuit that controls a cockpit warning light for certain
combinations of engine conditions. Assume that a HIGH at output W activates the
warning light.
i. Write Boolean function for W.
ii. Determine what engine conditions will give a warning to the pilot.
T
Temp
sonsor
Prossure
Warning
light
sensor
R
RPM
sonsor
Transcribed Image Text:Q 3. An Indian jet aircraft employs a system for monitoring the RPM, pressure, and temperature values of its engines using sensors that operate as follows: RPM sensor output = 0 only when speed < 4600 rpm P sensor output = 0 only when pressure < 210 psi T sensor output = (0 only when temperature < 180°F Figure shows the logic circuit that controls a cockpit warning light for certain combinations of engine conditions. Assume that a HIGH at output W activates the warning light. i. Write Boolean function for W. ii. Determine what engine conditions will give a warning to the pilot. T Temp sonsor Prossure Warning light sensor R RPM sonsor
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