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m (Note about payload) |
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=== Parameter definitions === | === Parameter definitions === | ||
{| class="prettytable" | {| class="prettytable" | ||
|emptywt | !i.. | ||
|Inertia. Higher values result in slower rolls than lower values. | |||
|- | |||
!emptywt | |||
|The weight of the empty aircraft. | |The weight of the empty aircraft. | ||
|- | |- | ||
!pointmass | |||
|There can be any number of pointmasses. Each can also have a shape which - if present - causes an associated moment of inertia to be calculated based on the shape. Note that a cylinder is solid, a tube is hollow, a ball is solid and a sphere is hollow. | |There can be any number of pointmasses. Each can also have a shape which - if present - causes an associated moment of inertia to be calculated based on the shape. Note that a cylinder is solid, a tube is hollow, a ball is solid and a sphere is hollow. | ||
|} | |} | ||
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=== Notes === | === Notes === | ||
* <tt>emptywt + pointmasses + fuel = total weight</tt> | * <tt>emptywt + pointmasses + fuel = total weight</tt> | ||
* Fuel weight is defined in the [[JSBSim Propulsion|propulsion section]]. | |||
You can add the pointmasses to the Equipment > Fuel and payload dialog, by adding the following code (for each single pointmass) to your aircraft's -set.xml file: | |||
<syntaxhighlight lang="xml"> | |||
<payload> | |||
<weight> | |||
<name type="string">Passengers and crew</name> | |||
<weight-lb alias="/fdm/jsbsim/inertia/pointmass-weight-lbs[0]"/> | |||
<min-lb type="double">3000.0</min-lb> | |||
<max-lb type="double">90000.0</max-lb> | |||
</weight> | |||
</payload> | |||
</syntaxhighlight> | |||
{{JSBSim}} | {{JSBSim}} | ||
[[Category:JSBSim|Mass and balance]] | [[Category:JSBSim|Mass and balance]] | ||