Flight safety is significantly enhanced through redundancy. Examples of redundancy in small aircraft design include a co-pilot’s duplicate set of flight controls, an ignition system independent of the electrical system, and engines that continue to run if the alternator and battery fail. Even if the engine completely fails, the plane can still be safely landed as a glider [1]. In this problem, you will use probability analysis to show how redundancy in a valve system enhances the system’s reliability. As you do the calculations, assume that each valve’s function is independent of the other valves’ function. Before installing these valves in an aircraft, the test engineer subjected the valves to rigorous laboratory testing. Based on the experimental data, it was determined that the probabilities of each of the three valves functioning correctly are: Valve A: 92% Valve B: 94% Valve C: 93%
Flight safety is significantly enhanced through redundancy. Examples of redundancy in small aircraft design include a co-pilot’s duplicate set of flight controls, an ignition system independent of the electrical system, and engines that continue to run if the alternator and battery fail. Even if the engine completely fails, the plane can still be safely landed as a glider [1]. In this problem, you will use probability analysis to show how redundancy in a valve system enhances the system’s reliability. As you do the calculations, assume that each valve’s function is independent of the other valves’ function. Before installing these valves in an aircraft, the test engineer subjected the valves to rigorous laboratory testing. Based on the experimental data, it was determined that the probabilities of each of the three valves functioning correctly are: Valve A: 92% Valve B: 94% Valve C: 93%
MATLAB: An Introduction with Applications
6th Edition
ISBN:9781119256830
Author:Amos Gilat
Publisher:Amos Gilat
Chapter1: Starting With Matlab
Section: Chapter Questions
Problem 1P
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Flight safety is significantly enhanced through redundancy. Examples of redundancy in small aircraft design include a co-pilot’s duplicate set of flight controls, an ignition system independent of the electrical system, and engines that continue to run if the alternator and battery fail. Even if the engine completely fails, the plane can still be safely landed as a glider [1]. In this problem, you will use
- As you do the calculations, assume that each valve’s
function is independent of the other valves’ function. - Before installing these valves in an aircraft, the test engineer subjected the valves to rigorous laboratory testing. Based on the experimental data, it was determined that the probabilities of each of the three valves functioning correctly are:
- Valve A: 92%
- Valve B: 94%
- Valve C: 93%
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