G-induced loss of consciousness for fighter pilots

The goal of this project is to further the study of Gravity induced Loss of Consciousness in Fighter Pilots. G induced loss of consciousness or G-LOC is defined in aviation medicine as “a state of altered perception whereby one’s awareness of reality is absent due to a sudden, critical reduction of...

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主要作者: Foo, Jonathan Zhi Bao.
其他作者: Alastair Campbell Ritchie
格式: Final Year Project
語言:English
出版: 2009
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在線閱讀:http://hdl.handle.net/10356/15726
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spelling sg-ntu-dr.10356-157262023-03-04T19:37:28Z G-induced loss of consciousness for fighter pilots Foo, Jonathan Zhi Bao. Alastair Campbell Ritchie School of Mechanical and Aerospace Engineering DRNTU::Engineering::Bioengineering The goal of this project is to further the study of Gravity induced Loss of Consciousness in Fighter Pilots. G induced loss of consciousness or G-LOC is defined in aviation medicine as “a state of altered perception whereby one’s awareness of reality is absent due to a sudden, critical reduction of cerebral blood circulation caused by an increase in G force”. The G-LOC phenomenon is not a single event but a complicated series of events. It involves loss of vision, loss of other sensory input, loss of motor output, loss of memory and loss of consciousness subsequently followed by recovery of these faculties. As G-LOC is one of the main factors contributing to aviation accidents resulting in loss of pilot lives and aircraft worth millions of dollars, there is a strong interest in this research. Furthermore, with the advancements in aviation technology resulting in aircrafts with a higher speed performance and ability to operate in higher pressure altitude condition, there is increased urgency in the study of G-LOC. The model created in this project was a modification of the Windkessel theory. It is an electric circuit analogy of the circulatory system, with parameters and elements to simulate the physiological responses of the human body when subjected to increasing G-loading. The input was a human’s aortic pressure waveform reconstructed from the first 10 harmonics using fourier series. 6 models with different parameters were created. Model 1 varies fluid resistance of the cerebral circulation with +Gz while Model 2 varies abdominal resistance to varying +Gz. Model 3 is the combination of Model 1 and 2. Model 4 and 5 are variations on the abdominal resistance to G-loading. Model 6 includes the baroreflex mechanism from the activation of baroreceptors for complete analysis under G-loading, predicting critical values of A-LOC, G-LOC and cell death occurring at 3.3G, 5G and 9G respectively. Using data from Model 6, the relationship between cerebral blood flow and the G-load factor could be established. Bachelor of Engineering (Mechanical Engineering) 2009-05-14T03:18:52Z 2009-05-14T03:18:52Z 2009 2009 Final Year Project (FYP) http://hdl.handle.net/10356/15726 en Nanyang Technological University 74 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Bioengineering
spellingShingle DRNTU::Engineering::Bioengineering
Foo, Jonathan Zhi Bao.
G-induced loss of consciousness for fighter pilots
description The goal of this project is to further the study of Gravity induced Loss of Consciousness in Fighter Pilots. G induced loss of consciousness or G-LOC is defined in aviation medicine as “a state of altered perception whereby one’s awareness of reality is absent due to a sudden, critical reduction of cerebral blood circulation caused by an increase in G force”. The G-LOC phenomenon is not a single event but a complicated series of events. It involves loss of vision, loss of other sensory input, loss of motor output, loss of memory and loss of consciousness subsequently followed by recovery of these faculties. As G-LOC is one of the main factors contributing to aviation accidents resulting in loss of pilot lives and aircraft worth millions of dollars, there is a strong interest in this research. Furthermore, with the advancements in aviation technology resulting in aircrafts with a higher speed performance and ability to operate in higher pressure altitude condition, there is increased urgency in the study of G-LOC. The model created in this project was a modification of the Windkessel theory. It is an electric circuit analogy of the circulatory system, with parameters and elements to simulate the physiological responses of the human body when subjected to increasing G-loading. The input was a human’s aortic pressure waveform reconstructed from the first 10 harmonics using fourier series. 6 models with different parameters were created. Model 1 varies fluid resistance of the cerebral circulation with +Gz while Model 2 varies abdominal resistance to varying +Gz. Model 3 is the combination of Model 1 and 2. Model 4 and 5 are variations on the abdominal resistance to G-loading. Model 6 includes the baroreflex mechanism from the activation of baroreceptors for complete analysis under G-loading, predicting critical values of A-LOC, G-LOC and cell death occurring at 3.3G, 5G and 9G respectively. Using data from Model 6, the relationship between cerebral blood flow and the G-load factor could be established.
author2 Alastair Campbell Ritchie
author_facet Alastair Campbell Ritchie
Foo, Jonathan Zhi Bao.
format Final Year Project
author Foo, Jonathan Zhi Bao.
author_sort Foo, Jonathan Zhi Bao.
title G-induced loss of consciousness for fighter pilots
title_short G-induced loss of consciousness for fighter pilots
title_full G-induced loss of consciousness for fighter pilots
title_fullStr G-induced loss of consciousness for fighter pilots
title_full_unstemmed G-induced loss of consciousness for fighter pilots
title_sort g-induced loss of consciousness for fighter pilots
publishDate 2009
url http://hdl.handle.net/10356/15726
_version_ 1759858263579426816