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PART B: Design Problem using Karnaugh Mapping Technique A 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 < 4800 rpm P sensor output = 0, when pressure <220 psi T sensor output = 0, only when temperature < 200°F Figure 2.1 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: (a) Create your truth Table with appropriate input-output combinations (b) Determine what engine conditions will give warning to the pilot. (c) Using K-Map technique to obtain your simplified Boolean equation. (d) Change this circuit to one using all NAND gates and constructs the circuit. Temp Sensor Pressure Sensor RPM Sensor T P R Figure 2.1 W Warning Light

PART B: Design Problem using Karnaugh Mapping Technique A 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 < 4800 rpm P sensor output = 0, when pressure <220 psi T sensor output = 0, only when temperature < 200°F Figure 2.1 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: (a) Create your truth Table with appropriate input-output combinations (b) Determine what engine conditions will give warning to the pilot. (c) Using K-Map technique to obtain your simplified Boolean equation. (d) Change this circuit to one using all NAND gates and constructs the circuit. Temp Sensor Pressure Sensor RPM Sensor T P R Figure 2.1 W Warning Light

Introductory Circuit Analysis (13th Edition)
Introductory Circuit Analysis (13th Edition)
13th Edition
ISBN:9780133923605
Author:Robert L. Boylestad
Publisher:Robert L. Boylestad
Chapter1: Introduction
Section: Chapter Questions
Problem 1P: Visit your local library (at school or home) and describe the extent to which it provides literature...
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PART B: Design Problem using Karnaugh Mapping Technique A 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 < 4800 rpm P sensor output = 0, when pressure <220 psi T sensor output = 0, only when temperature < 200°F Figure 2.1 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: (a) Create your truth Table with appropriate input-output combinations. (b) Determine what engine conditions will give warning to the pilot. (c) Using K-Map technique to obtain your simplified Boolean equation. (d) Change this circuit to one using all NAND gates and constructs the circuit. Temp Sensor DIGITAL ELECTRONICS STB 24403 Pressure Sensor RPM Sensor P R Figure 2.1 W Warning Light
Transcribed Image Text:PART B: Design Problem using Karnaugh Mapping Technique A 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 < 4800 rpm P sensor output = 0, when pressure <220 psi T sensor output = 0, only when temperature < 200°F Figure 2.1 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: (a) Create your truth Table with appropriate input-output combinations. (b) Determine what engine conditions will give warning to the pilot. (c) Using K-Map technique to obtain your simplified Boolean equation. (d) Change this circuit to one using all NAND gates and constructs the circuit. Temp Sensor DIGITAL ELECTRONICS STB 24403 Pressure Sensor RPM Sensor P R Figure 2.1 W Warning Light
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