Take-off performance analysis method, electronic equipment and storage medium
The invention discloses a take-off performance analysis method which comprises the following steps: receiving a calculation condition combination sent by a terminal, the calculation condition combination comprising an external temperature; Performing matching according to the external temperature an...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The invention discloses a take-off performance analysis method which comprises the following steps: receiving a calculation condition combination sent by a terminal, the calculation condition combination comprising an external temperature; Performing matching according to the external temperature and the weight limiting table to obtain the corresponding maximum load capacity; When the corresponding external temperature data does not exist in the weight limiting table, obtaining a temperature interval to which the external temperature belongs, obtaining a temperature value and a weight value corresponding to the two ends of the temperature interval, and performing difference calculation according to the temperature value and the weight value to obtain the maximum load capacity correspondingto the external temperature; And obtaining a performance calculation mode matched with the calculation condition combination according to the maximum load capacity to obtain aircraft performance data. The invention further p |
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