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Docs for the solution fuel and solve-weight features.

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andy 2004-02-18 15:39:36 +00:00
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Aircraft-yasim/README.yasim
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@ -21,6 +21,7 @@ approach: The approach parameters for the aircraft. The solver will
approach. approach.
speed: The approach airspeed, in knots TAS. speed: The approach airspeed, in knots TAS.
aoa: The approach angle of attack, in degrees aoa: The approach angle of attack, in degrees
fuel: Fraction (0-1) of fuel in the tanks. Default is 0.2.
cruise: The cruise speed and altitude for the solver to match. As cruise: The cruise speed and altitude for the solver to match. As
above, this should contain <control> elements indicating above, this should contain <control> elements indicating
@ -28,6 +29,7 @@ cruise: The cruise speed and altitude for the solver to match. As
are generating enough thrust at cruise! are generating enough thrust at cruise!
speed: The cruise speed, in knots TAS. speed: The cruise speed, in knots TAS.
alt: The cruise altitude, in feet MSL. alt: The cruise altitude, in feet MSL.
fuel: Fraction (0-1) of fuel in the tanks. Default is 0.2.
cockpit: The location of the cockpit (pilot eyepoint). cockpit: The location of the cockpit (pilot eyepoint).
x,y,z: eyepoint location (see coordinates note) x,y,z: eyepoint location (see coordinates note)
@ -282,6 +284,15 @@ weight: This is an added weight, something not part of the empty
which results in no aerodynamic force (internal which results in no aerodynamic force (internal
cargo). cargo).
solve-weight:
Subtag of approach and cruise parameters. Used to specify a
non-zero setting for a <weight> tag during solution. The
default is to assume all weights are zero at the given
performance numbers.
idx: Index of the weight in the file (starting with zero).
weight: Weight setting in pounds.
control: This element, which can appear in two different contexts, control: This element, which can appear in two different contexts,
manages a mapping from fgfs properties (user input) to manages a mapping from fgfs properties (user input) to
settable values on the aircraft's objects. Note that the settable values on the aircraft's objects. Note that the