FIELD: aircraft equipment. SUBSTANCE: method involves generation of boundaries of turbulent thunderstorm region which has thunderstorm core, turbulent region around thunderstorm core with heavy and medium turbulence which decreases towards region boundaries with probability of 20 % which is determined by probability of error in detection of thunderstorm core. In addition method involves generation of turbulent thunderstorm edge as set of intersecting turbulent thunderstorm regions which are increased by factor of 1.6 with respect to calculated values because turbulence frequency conforms to condition of sum of turbulence in adjacent thunderstorm cores. This results in generation and displaying of boundaries of both turbulence thunderstorm region and turbulence thunderstorm edge. EFFECT: increased functional capabilities. 1 dwg
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Authors
Dates
1997-12-27—Published
1996-01-10—Filed