Framework for the estimation of safe wake separation distance between same-track multi-rotor UAS
As the surface traffic in modern cities becomes more congested, people turn to the vertical dimension to accommodate the projected increase in urban population density. In order to facilitate the utilization of the urban airspace for passenger and cargo transportation, however, a safe and efficient...
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sg-ntu-dr.10356-1466402021-03-06T20:10:21Z Framework for the estimation of safe wake separation distance between same-track multi-rotor UAS Wang, John Chung-Hung Nathanael, Joshua C. Ng, Ee Meng Ng, Bing Feng Low, Kin Huat AIAA SciTech 2021 Forum Air Traffic Management Research Institute Engineering::Aeronautical engineering::Aviation Unmanned Aircraft System Wake Vortex As the surface traffic in modern cities becomes more congested, people turn to the vertical dimension to accommodate the projected increase in urban population density. In order to facilitate the utilization of the urban airspace for passenger and cargo transportation, however, a safe and efficient method of managing these traffic is needed. Several UAS (Unmanned Aircraft System) Traffic Management (UTM) concept of operations have been proposed and studied by various research agencies around the world to address this need, though hard data needed to validate the safety assessment of said concepts is lacking. The current paper proposes a hybridComputational Fluid Dynamics (CFD)-Flight Dynamics simulationworkflow to analyze the necessity of wake-vortex based separation standard for multi-rotor air-vehicles within the UTM controlled airspace. This is accomplished through the usage of Virtual Blade Model (VBM) to simplify the simulation of near-field wake of the multi-rotor air-vehicle, which is mapped into the LES domain to generate the wake-field that the SIMULINK flight dynamics model would use to generate the wake-encounter response of a follower multi-rotor air-vehicle The outlined workflow could be used to estimate the attitude of the follower vehicle and the associate rate of change for a given encounter-pair at various separation distance, which could eventually contribute, along with other factors such as navigational uncertainties etc., to the establishment of required-sizing for safety “bubble” around an UAS. This safe-separation requirement would impact the safety assessment and the overall capacity of the UTM system. Civil Aviation Authority of Singapore (CAAS) Accepted version This project is supported by the Civil Aviation Authority of Singapore and the Nanyang Technological University, Singapore under their collaboration in the Air Traffic Management Research Institute. Any opinions, findings and conclusions or recommendations expressed in this material are those of the authors and do not reflect the views of the Civil Aviation Authority of Singapore. 2021-03-04T01:58:58Z 2021-03-04T01:58:58Z 2021 Conference Paper Wang, J. C.-H., Nathanael, J. C., Ng, E. M., Ng, B. F., & Low, K. H. (2021). Framework for the estimation of safe wake separation distance between same-track multi-rotor UAS. Proceedings of the AIAA SciTech 2021 Forum. doi:10.2514/6.2021-0708 978-1-62410-609-5 https://hdl.handle.net/10356/146640 10.2514/6.2021-0708 en © 2021 Nanyang Technological University. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. application/pdf |
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Engineering::Aeronautical engineering::Aviation Unmanned Aircraft System Wake Vortex Wang, John Chung-Hung Nathanael, Joshua C. Ng, Ee Meng Ng, Bing Feng Low, Kin Huat Framework for the estimation of safe wake separation distance between same-track multi-rotor UAS |
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As the surface traffic in modern cities becomes more congested, people turn to the vertical dimension to accommodate the projected increase in urban population density. In order to facilitate the utilization of the urban airspace for passenger and cargo transportation, however, a safe and efficient method of managing these traffic is needed. Several UAS (Unmanned Aircraft System) Traffic Management (UTM) concept of operations have been proposed and studied by various research agencies around the world to address this need, though hard data needed to validate the safety assessment of said concepts is lacking. The current paper proposes a hybridComputational Fluid Dynamics (CFD)-Flight Dynamics simulationworkflow to analyze the necessity of wake-vortex based separation standard for multi-rotor air-vehicles within the UTM controlled airspace. This is accomplished through the usage of Virtual Blade Model (VBM) to simplify the simulation of near-field wake of the multi-rotor air-vehicle, which is mapped into the LES domain to generate the wake-field that the SIMULINK flight dynamics model would use to generate the wake-encounter response of a follower multi-rotor air-vehicle The outlined workflow could be used to estimate the attitude of the follower vehicle and the associate rate of change for a given encounter-pair at various separation distance, which could eventually contribute, along with other factors such as navigational uncertainties etc., to the establishment of required-sizing for safety “bubble” around an UAS. This safe-separation requirement would impact the safety assessment and the overall capacity of the UTM system. |
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AIAA SciTech 2021 Forum |
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AIAA SciTech 2021 Forum Wang, John Chung-Hung Nathanael, Joshua C. Ng, Ee Meng Ng, Bing Feng Low, Kin Huat |
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Conference or Workshop Item |
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Wang, John Chung-Hung Nathanael, Joshua C. Ng, Ee Meng Ng, Bing Feng Low, Kin Huat |
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Wang, John Chung-Hung |
title |
Framework for the estimation of safe wake separation distance between same-track multi-rotor UAS |
title_short |
Framework for the estimation of safe wake separation distance between same-track multi-rotor UAS |
title_full |
Framework for the estimation of safe wake separation distance between same-track multi-rotor UAS |
title_fullStr |
Framework for the estimation of safe wake separation distance between same-track multi-rotor UAS |
title_full_unstemmed |
Framework for the estimation of safe wake separation distance between same-track multi-rotor UAS |
title_sort |
framework for the estimation of safe wake separation distance between same-track multi-rotor uas |
publishDate |
2021 |
url |
https://hdl.handle.net/10356/146640 |
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