4.1 Article

On Low Altitude Flight Through The Atmospheric Boundary Layer

Journal

INTERNATIONAL JOURNAL OF MICRO AIR VEHICLES
Volume 2, Issue 2, Pages 55-68

Publisher

SAGE PUBLICATIONS LTD
DOI: 10.1260/1756-8293.2.2.55

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Funding

  1. United States Air Force Research Laboratory via the Asian Office of Aerospace Research and Development

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Major challenges to low speed micro flight are the transient and time-averaged velocities arising from the Atmospheric Boundary Layer (ABL), particularly turbulence a few metres above the ground. In this paper, existing data from meteorologists and wind engineers are reviewed and measurements dedicated to understanding the spatial and temporal velocity fields that MAVs experience are briefly described. Data from a wide variety of terrains are analysed, with the majority of data obtained in relatively well mixed turbulent flow (i.e. away from local effects such as buildings) and for conditions of nominally neutral stability. Spectra for data well removed from local effects exhibited the expected 5/3rds Kolmogorov law. Transient flow pitch angles were investigated (obtained from four small laterally displaced probes), in order to understand the possible roll and pitch inputs to MAVs. It was noted that for all data obtained the variation with lateral separation decreased relatively slowly with reducing separation down to the closest inter-probe spacing of 14mm. This effect is thought to explain the increasing piloting difficulties experienced in maintaining good roll control for decreasing scales of craft when any appreciable atmospheric winds are present.

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