QUANTIFICATION OF CONTROLLED FLIGHT INTO TERRAIN ACCIDENT PROBABILITY BASED ON FLIGHT OPERATIONAL DATA

Aviation safety is always improving. However, current methods can only evaluate the safety carried on past operations. As a result, there is a need for models that can predict how likely it is for airplanes to get into accidents. This need is even stronger now that individual airlines must set their...

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Main Author: Aulia Soegiharto, Fikri
Format: Theses
Language:Indonesia
Subjects:
Online Access:https://digilib.itb.ac.id/gdl/view/84395
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Institution: Institut Teknologi Bandung
Language: Indonesia
id id-itb.:84395
spelling id-itb.:843952024-08-15T12:27:18ZQUANTIFICATION OF CONTROLLED FLIGHT INTO TERRAIN ACCIDENT PROBABILITY BASED ON FLIGHT OPERATIONAL DATA Aulia Soegiharto, Fikri Teknik (Rekayasa, enjinering dan kegiatan berkaitan) Indonesia Theses Acceptable Level of Safety Performance, Controlled Flight into Terrain, Predictive, Simulations. INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/84395 Aviation safety is always improving. However, current methods can only evaluate the safety carried on past operations. As a result, there is a need for models that can predict how likely it is for airplanes to get into accidents. This need is even stronger now that individual airlines must set their own Acceptable Level of Safety Performance (ALoSP). This study investigates the relation between contributing factors identified through an aircraft physics model for Controlled Flight into Terrain (CFIT) events. The model incorporates propulsive, gravitational, and aerodynamic forces acting on the aircraft based on incident-free flight data. Contributing factors are extracted from the data to establish their probability distribution. These factors are then integrated into the model to compute the probability of CFIT using Subset Simulation. The Subset Simulation results yield a probability value of 1.20E-04 for CFIT events. After the probability is obtained, a sensitivity analysis is conducted to identify the factor contributing most significantly to CFIT events. It is found that flight path angle is the most influential contributing factor. Based on these insights, airlines are recommended to implement a target flight path angle of -3° during approach to enhance operational safety and potentially mitigate future CFIT occurrences. text
institution Institut Teknologi Bandung
building Institut Teknologi Bandung Library
continent Asia
country Indonesia
Indonesia
content_provider Institut Teknologi Bandung
collection Digital ITB
language Indonesia
topic Teknik (Rekayasa, enjinering dan kegiatan berkaitan)
spellingShingle Teknik (Rekayasa, enjinering dan kegiatan berkaitan)
Aulia Soegiharto, Fikri
QUANTIFICATION OF CONTROLLED FLIGHT INTO TERRAIN ACCIDENT PROBABILITY BASED ON FLIGHT OPERATIONAL DATA
description Aviation safety is always improving. However, current methods can only evaluate the safety carried on past operations. As a result, there is a need for models that can predict how likely it is for airplanes to get into accidents. This need is even stronger now that individual airlines must set their own Acceptable Level of Safety Performance (ALoSP). This study investigates the relation between contributing factors identified through an aircraft physics model for Controlled Flight into Terrain (CFIT) events. The model incorporates propulsive, gravitational, and aerodynamic forces acting on the aircraft based on incident-free flight data. Contributing factors are extracted from the data to establish their probability distribution. These factors are then integrated into the model to compute the probability of CFIT using Subset Simulation. The Subset Simulation results yield a probability value of 1.20E-04 for CFIT events. After the probability is obtained, a sensitivity analysis is conducted to identify the factor contributing most significantly to CFIT events. It is found that flight path angle is the most influential contributing factor. Based on these insights, airlines are recommended to implement a target flight path angle of -3° during approach to enhance operational safety and potentially mitigate future CFIT occurrences.
format Theses
author Aulia Soegiharto, Fikri
author_facet Aulia Soegiharto, Fikri
author_sort Aulia Soegiharto, Fikri
title QUANTIFICATION OF CONTROLLED FLIGHT INTO TERRAIN ACCIDENT PROBABILITY BASED ON FLIGHT OPERATIONAL DATA
title_short QUANTIFICATION OF CONTROLLED FLIGHT INTO TERRAIN ACCIDENT PROBABILITY BASED ON FLIGHT OPERATIONAL DATA
title_full QUANTIFICATION OF CONTROLLED FLIGHT INTO TERRAIN ACCIDENT PROBABILITY BASED ON FLIGHT OPERATIONAL DATA
title_fullStr QUANTIFICATION OF CONTROLLED FLIGHT INTO TERRAIN ACCIDENT PROBABILITY BASED ON FLIGHT OPERATIONAL DATA
title_full_unstemmed QUANTIFICATION OF CONTROLLED FLIGHT INTO TERRAIN ACCIDENT PROBABILITY BASED ON FLIGHT OPERATIONAL DATA
title_sort quantification of controlled flight into terrain accident probability based on flight operational data
url https://digilib.itb.ac.id/gdl/view/84395
_version_ 1822998547798163456