PART-1 Combinational Logic Design A jet aircraft employs a system for monitoring rpm, pressure, and temperature values of its engines using sensors that operate as follows: R: RPM sensor output = 0 when speed < 4800 rpm P: Pressure sensor output = 0 when pressure < 220 psi T: Temperature sensor output = 0 when temperature < 200°F The output warning W is activated (i.e. logic '1') when any of these conditions occur 1. Temperature > 200°F and pressure > 220 psi 2. Pressure < 220 psi, but temperature > 200°F and rpm < 4800 rpm Other than these conditions, the output W is deactivated (i.e. logic 'o'). You are tasked with designing the combinational logic part of the system, where the output warning light W will be sent to an LED for real-time monitoring based on the sensor inputs R, P, and T. а. Derive the truth table for the design b. Using Karnaugh-Maps, derive the Boolean equation with the minimum number of literals С. Draw the minimized circuit in part (b) using basic gates (NOT, AND, OR)

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PART-1 Combinational Logic Design
A jet aircraft employs a system for monitoring rpm, pressure, and temperature values of its engines
using sensors that operate as follows:
R: RPM sensor output = 0 when speed < 4800 rpm
P: Pressure sensor output = 0 when pressure < 220 psi
T: Temperature sensor output = 0 when temperature < 200°F
The output warning W is activated (i.e. logic '1') when any of these conditions occur
1. Temperature > 200°F and pressure > 220 psi
2. Pressure < 220 psi, but temperature > 200°F and rpm < 4800 rpm
Other than these conditions, the output W is deactivated (i.e. logic 'o').
You are tasked with designing the combinational logic part of the system, where the output warning
light W will be sent to an LED for real-time monitoring based on the sensor inputs R, P, and T.
а.
Derive the truth table for the design
b. Using Karnaugh-Maps, derive the Boolean equation with the minimum number of literals
)
C.
Draw the minimized circuit in part (b) using basic gates (NOT, AND, OR)
d. Redraw the minimized circuit in part (b) using universal gates (NOT, NAND, NOR)
e. Assume the output warning W is activated only when condition (1) occurs (i.e. Temperature
> 200°F and pressure > 220 psi). Is the new logic circuit more simplified or more complex
than the original logic circuit? In your opinion, why is this?
Transcribed Image Text:PART-1 Combinational Logic Design A jet aircraft employs a system for monitoring rpm, pressure, and temperature values of its engines using sensors that operate as follows: R: RPM sensor output = 0 when speed < 4800 rpm P: Pressure sensor output = 0 when pressure < 220 psi T: Temperature sensor output = 0 when temperature < 200°F The output warning W is activated (i.e. logic '1') when any of these conditions occur 1. Temperature > 200°F and pressure > 220 psi 2. Pressure < 220 psi, but temperature > 200°F and rpm < 4800 rpm Other than these conditions, the output W is deactivated (i.e. logic 'o'). You are tasked with designing the combinational logic part of the system, where the output warning light W will be sent to an LED for real-time monitoring based on the sensor inputs R, P, and T. а. Derive the truth table for the design b. Using Karnaugh-Maps, derive the Boolean equation with the minimum number of literals ) C. Draw the minimized circuit in part (b) using basic gates (NOT, AND, OR) d. Redraw the minimized circuit in part (b) using universal gates (NOT, NAND, NOR) e. Assume the output warning W is activated only when condition (1) occurs (i.e. Temperature > 200°F and pressure > 220 psi). Is the new logic circuit more simplified or more complex than the original logic circuit? In your opinion, why is this?
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