Wind tunnel testing is done first to establish the aerodynamic characteristics of the dropwindsonde body alone and the dropwindsonde body plus parachute. Combining this information with the full non-linear equations of motion for a falling body and an appropriate numerical method for generating an artificial random wind field using a second order autoregressive process to form auto- and cross-correlation matrices allows a model of the behaviour of the falling dropwindsonde in a turbulent atmospheric boundary layer to be developed. This allows the effects of the linearization of the wind finding equations and the conditions under which they may not be valid to be explored. In addition, relationships between both individual and composited observed' dropwindsonde profiles and the simulated boundary layer characteristics can be obtained to assist the understanding of actual observed dropwindsonde profiles.
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