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Quantification of Uncertainty and Risk Sensitivity for Safety of Emerging Operations The growing need to develop and deploy small unmanned aerial vehicles (sUAVs) for various applications in the airspace necessitates reliable tools to accurately predict the flight trajectories of the sUAVs. The knowledge of the predicted trajectories help decision makers anticipate potential conflict, assess the risk, and take appropriate risk mitigation actions. In addition, uncertainties in vehicle models, weather, and controller action further highlights the need for reliable prediction tools.
In this project, the application of mixed sparse grid-based quadrature and generalized polynomial chaos(gPC) expansion method for uncertainty quantification and collision assessment in air traffic consisting of fixed-wing small unmanned aerial vehicles (sUAV) was studied. From the results obtained, it can be concluded that this provides a reliable framework to carry out quantitative conflict assessment in an unmanned air traffic, which when employed, can improve the functionalities of the unmanned traffic management system. It was observed that the results from the gPC expansion framework developed in the project can be utilized to conduct rapid probabilistic collision assessment for near real-time unmanned traffic management in the airspace. From the vehicle models, position updates, and wind-field data, a priori gPC based 3-σcon-fidence ellipses can provide estimates of potential conflict at some future instants. The computational costs scaled linearly when the uncertain inputs were fewer. Further, the largest allowable distribution of para-metric uncertainties that leads to the smallest risk of collision in traffic of small unmanned aerial vehicles could be calculated. The time of closest approach between two sUAVs can be established paving way for development of proactive mitigation strategies. The separation between the sUAVs was found to be most significantly affected by uncertainties in the maximum available thrusts, zero-lift drag coefficients, and wing planform areas of the sUAVs. The study of uncertain wind-fields indicated that a heterogeneous traffic mix resulted in an increased probability of conflict. Increased measurement update rate reduced the uncertain-ties in the trajectories of the vehicles, further reducing the probability of conflict but rapid updates of all vehicles in the airspace poses a stringent communication limitation. The gPC framework also provided the means to analyze vehicle impact (crash region) due to loss of control resulting from actuator failure in sUAS traffic, essentially to predict impact and crash zones for representative vehicles. The predicted regions when compared with non-participant density, provides a means to develop an early mitigation strategy, should the sUAV detect an imminent actuator failure.
Document ID
20240013241
Acquisition Source
Ames Research Center
Document Type
Technical Publication (TP)
Authors
Rajnish Bhusal
(The University of Texas at Arlington Arlington, Texas, United States)
Aakarshan Khanal
(The University of Texas at Arlington Arlington, Texas, United States)
Kamesh Subbarao
(The University of Texas at Arlington Arlington, Texas, United States)
Animesh Chakravarthy
(The University of Texas at Arlington Arlington, Texas, United States)
Wendy A Okolo
(Ames Research Center Mountain View, United States)
Date Acquired
October 18, 2024
Publication Date
October 1, 2024
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Earth Resources and Remote Sensing
Space Transportation and Safety
Aircraft Design, Testing and Performance
Report/Patent Number
NASA/TP-20240013241
Funding Number(s)
CONTRACT_GRANT: 80NSSC21K1508 P00001
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
NASA Peer Committee
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