Compute weight and balance for your aircraft.

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<p>Setup custom weight and balance calculator for your aircraft. Given weight,<br />
and fuel quantity computes whether the aircraft is within limits and plots<br />
where current loading is on the loading envelope.</p>
<h4>Shortcode Usage</h4>
<p>[weight_and_balance wb_empty_weight=lbs wb_empty_arm=inch-lbs wb_A_arm=lbs<br />
wb_B_arm=inch-lbs wb_C_arm=inch-lbs wb_fuel_arm=inch-lbs wb_fuel_weight=galons wb_bounding_box=”arm,moment arm,moment …”]</p>
<p>Shortcode arguments:</p>
<ul>
<li>Empty weight and arm: wb_empty_weight=lbs and wb_emty_arm=inch-lbs</li>
<li>Any number of loading arms: wb_<em></em><em>arm and optional default weight for each wb</em>_weight. The weight can be expressed as an expression which is useful for fuel, eg 44*6 as a default weight means 44 gallons times 6 pounds per gallon.</li>
<li>A bounding box: Space separated list of arm,moment that describes the acceptable limits. wb_bounding_box=”arm,moment …”</li>
</ul>
<p>Example:<br />
[weight_and_balance wb_empty_weight=1519.75 wb_empty_arm=83.02 wb_front_arm=90.6 wb_rear_arm=126 wb_fuel_arm=94.8 wb_fuel_weight=52*6 wb_bounding_box=”124,1525 156,1925 214,2400 222,2400 140,1525″]</p>
<h3>Disclaimer</h3>
<p>Use at your own risk.</p>


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