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(→wing) |
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Line 5: | Line 5: | ||
==== airplane ==== | ==== airplane ==== | ||
The top-level element for the file. It contains only one attribute: | The top-level element for the file. It contains only one attribute: | ||
*'''mass:''' The empty (no fuel) weight, in pounds. | *'''mass:''' The empty (no fuel) weight, in pounds. It does include the weight of the engine(s), so when you add the engine weight in its tag, it acts just like a ballast. | ||
==== approach ==== | ==== approach ==== | ||
The approach parameters for the aircraft. The solver will generate an aircraft that matches these settings. The element can (and should) contain <control> elements indicating pilot input settings, such as flaps and throttle, for the approach. | The approach parameters for the aircraft. The solver will generate an aircraft that matches these settings. The element can (and should) contain <control> elements indicating pilot input settings, such as flaps and throttle, for the approach. |
edits