Quantitative reliability and airworthiness analysis of propulsion systems of multi-rotor UAVs for certification in civil airspace
Unmanned Aerial Vehicles (UAVs) have become increasingly integral to a diverse array of industrial applications, including military, civilian, and commercial uses. Ensuring their airworthiness is critical for the safe and effective operation of UAVs. This necessitates advancements in sophisticated u...
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sg-ntu-dr.10356-1820452025-01-11T16:54:17Z Quantitative reliability and airworthiness analysis of propulsion systems of multi-rotor UAVs for certification in civil airspace Govind, Siddesh Mir Feroskhan School of Mechanical and Aerospace Engineering Air Traffic Management Research Institute mir.feroskhan@ntu.edu.sg Engineering UAV reliability Airworthiness certification Multi-rotor UAVs Propulsion systems Failure mode and effects analysis (FMEA) Markov chains Degradation modelling Weibull analysis Predictive maintenance Unmanned aerial vehicles (UAVs Urban air mobility (UAM) Bayesian modelling Deep learning in UAVs LSTM networks Reliability engineering Drone performance evaluation Experimental testbeds Component-level analysis System-level reliability Predictive modelling Unmanned Aerial Vehicles (UAVs) have become increasingly integral to a diverse array of industrial applications, including military, civilian, and commercial uses. Ensuring their airworthiness is critical for the safe and effective operation of UAVs. This necessitates advancements in sophisticated urban air traffic management strategies and the implementation of robust evaluation tools. Assessing UAV airworthiness requires a detailed examination of their reliability or health state, utilizing available data and model-based evaluation criteria. Evaluating the reliability of UAVs involves analysing their capacity to perform designated functions reliably, safely, and efficiently over a specified period. This critical evaluation requires continuous monitoring and analysis of data pertaining to the UAV’s operational performance, including indicators such as reliability, maintainability, and availability. In this context, this thesis explores and establishes diverse methodologies adaptable to various scenarios, considering the format and quantity of available source data. By employing both statistical and data-driven approaches, the research developed models for assessing the reliability and performance degradation of UAVs at both the component and system levels. Through FMEA, critical failure modes in UAV propulsion systems were identified, revealing that motor failures account for approximately 45% of total failures. Weibull analysis predicted motor failures with a 90% confidence interval, highlighting wear-out mechanisms as predominant. Additionally, LSTM-based models for predicting UAV performance degradation achieved an accuracy of 85% in forecasting remaining useful life (RUL). These models demonstrated significant potential in enhancing predictive maintenance strategies, reducing downtime by up to 30%, and improving the overall reliability and safety of UAV operations. This work aims to refine UAV airworthiness evaluation methodologies, ensuring their safe integration and operation in complex airspace systems. Master's degree 2025-01-06T06:42:23Z 2025-01-06T06:42:23Z 2024 Thesis-Master by Research Govind, S. (2024). Quantitative reliability and airworthiness analysis of propulsion systems of multi-rotor UAVs for certification in civil airspace. Master's thesis, Nanyang Technological University, Singapore. https://hdl.handle.net/10356/182045 https://hdl.handle.net/10356/182045 en This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License (CC BY-NC 4.0). application/pdf Nanyang Technological University |
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Engineering UAV reliability Airworthiness certification Multi-rotor UAVs Propulsion systems Failure mode and effects analysis (FMEA) Markov chains Degradation modelling Weibull analysis Predictive maintenance Unmanned aerial vehicles (UAVs Urban air mobility (UAM) Bayesian modelling Deep learning in UAVs LSTM networks Reliability engineering Drone performance evaluation Experimental testbeds Component-level analysis System-level reliability Predictive modelling |
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Engineering UAV reliability Airworthiness certification Multi-rotor UAVs Propulsion systems Failure mode and effects analysis (FMEA) Markov chains Degradation modelling Weibull analysis Predictive maintenance Unmanned aerial vehicles (UAVs Urban air mobility (UAM) Bayesian modelling Deep learning in UAVs LSTM networks Reliability engineering Drone performance evaluation Experimental testbeds Component-level analysis System-level reliability Predictive modelling Govind, Siddesh Quantitative reliability and airworthiness analysis of propulsion systems of multi-rotor UAVs for certification in civil airspace |
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Unmanned Aerial Vehicles (UAVs) have become increasingly integral to a diverse array of industrial applications, including military, civilian, and commercial uses. Ensuring their airworthiness is critical for the safe and effective operation of UAVs. This necessitates advancements in sophisticated urban air traffic management strategies and the implementation of robust evaluation tools. Assessing UAV airworthiness requires a detailed examination of their reliability or health state, utilizing available data and model-based evaluation criteria.
Evaluating the reliability of UAVs involves analysing their capacity to perform designated functions reliably, safely, and efficiently over a specified period. This critical evaluation requires continuous monitoring and analysis of data pertaining to the UAV’s operational performance, including indicators such as reliability, maintainability, and availability.
In this context, this thesis explores and establishes diverse methodologies adaptable to various scenarios, considering the format and quantity of available source data. By employing both statistical and data-driven approaches, the research developed models for assessing the reliability and performance degradation of UAVs at both the component and system levels. Through FMEA, critical failure modes in UAV propulsion systems were identified, revealing that motor failures account for approximately 45% of total failures. Weibull analysis predicted motor failures with a 90% confidence interval, highlighting wear-out mechanisms as predominant. Additionally, LSTM-based models for predicting UAV performance degradation achieved an accuracy of 85% in forecasting remaining useful life (RUL). These models demonstrated significant potential in enhancing predictive maintenance strategies, reducing downtime by up to 30%, and improving the overall reliability and safety of UAV operations. This work aims to refine UAV airworthiness evaluation methodologies, ensuring their safe integration and operation in complex airspace systems. |
author2 |
Mir Feroskhan |
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Mir Feroskhan Govind, Siddesh |
format |
Thesis-Master by Research |
author |
Govind, Siddesh |
author_sort |
Govind, Siddesh |
title |
Quantitative reliability and airworthiness analysis of propulsion systems of multi-rotor UAVs for certification in civil airspace |
title_short |
Quantitative reliability and airworthiness analysis of propulsion systems of multi-rotor UAVs for certification in civil airspace |
title_full |
Quantitative reliability and airworthiness analysis of propulsion systems of multi-rotor UAVs for certification in civil airspace |
title_fullStr |
Quantitative reliability and airworthiness analysis of propulsion systems of multi-rotor UAVs for certification in civil airspace |
title_full_unstemmed |
Quantitative reliability and airworthiness analysis of propulsion systems of multi-rotor UAVs for certification in civil airspace |
title_sort |
quantitative reliability and airworthiness analysis of propulsion systems of multi-rotor uavs for certification in civil airspace |
publisher |
Nanyang Technological University |
publishDate |
2025 |
url |
https://hdl.handle.net/10356/182045 |
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1821237183363678208 |