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)