AIAA SCITECH 2023 Forum 2023
DOI: 10.2514/6.2023-1012
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Comparison of Small Multirotor Wake Vortex of Different Weight Class and Rotor Configurations via Numerical Simulation

Abstract: Wake hazard is one of the factors affecting the separation requirement for same-track fixedwing aircraft in civil aviation. It could also be a contributing factor for UAS traffic management (UTM) with multirotors, especially with the widespread use of ADS-B like remoteID for UAS that greatly reduces the separation requirements due to communication, navigation, and surveillance (CNS) performance of the aircraft and the airspace. While the wake vortex structure and decay mechanism for fixed-wing aircraft has bee… Show more

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Cited by 1 publication
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“…In addition, instead of only inferring the wind effect from the flow results, the simulated wind data can be utilized for UAS flight simulation using software-in-the-loop (SITL) [27,28] to study UAS stability and flight behavior when encountering the flow patterns in the urban wind field. Simulation with SITL was previously used to determine the separation requirement between UAS by examining the flight behavior of UAS when encountering the wake vortex from another UAS [29,30].…”
Section: Summary and Future Workmentioning
confidence: 99%
“…In addition, instead of only inferring the wind effect from the flow results, the simulated wind data can be utilized for UAS flight simulation using software-in-the-loop (SITL) [27,28] to study UAS stability and flight behavior when encountering the flow patterns in the urban wind field. Simulation with SITL was previously used to determine the separation requirement between UAS by examining the flight behavior of UAS when encountering the wake vortex from another UAS [29,30].…”
Section: Summary and Future Workmentioning
confidence: 99%