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Add information on the control axis LACCEL. Correct typos.

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vmmeazza 2009-05-02 08:30:34 +00:00
parent 29541548b6
commit 7b24684016
1 changed files with 12 additions and 9 deletions
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Docs/README.yasim
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@ -370,7 +370,9 @@ gear: Defines a landing gear. Accepts <control> subelements to map
are not active on runways. Defaults to "0". You can are not active on runways. Defaults to "0". You can
not exclude all gears in the solving process. not exclude all gears in the solving process.
launchbar: Defines a catapult launchbar or strop. launchbar: Defines a catapult launchbar or strop. The default acceleration
provided by the catapult is 25m/s^2. This can be
modified by the use of the control axis LACCEL.
x,y,z: The location of the mount point of the launch bar or x,y,z: The location of the mount point of the launch bar or
strop on the aircraft. strop on the aircraft.
length: The length of the launch bar from mount point to tip length: The length of the launch bar from mount point to tip
@ -463,7 +465,7 @@ control-input:
FLAP0 - The flap0 deflection of a wing. FLAP0 - The flap0 deflection of a wing.
FLAP1 - The flap1 deflection of a wing. FLAP1 - The flap1 deflection of a wing.
FLAP[0/1]EFFECTIVENESS - a multiplier for flap lift, but not drag FLAP[0/1]EFFECTIVENESS - a multiplier for flap lift, but not drag
(useful for blown flaps (useful for blown flaps)
SLAT - The slat extension of a wing. SLAT - The slat extension of a wing.
SPOILER - The spoiler extension for a wing. SPOILER - The spoiler extension for a wing.
CYCLICAIL - The "aileron" cyclic input of a rotor CYCLICAIL - The "aileron" cyclic input of a rotor
@ -471,6 +473,7 @@ control-input:
COLLECTIVE - The collective input of a rotor COLLECTIVE - The collective input of a rotor
ROTORENGINEON - If not equal zero the rotor is rotating ROTORENGINEON - If not equal zero the rotor is rotating
WINCHRELSPEED - The relative winch speed WINCHRELSPEED - The relative winch speed
LACCEL - The acceleration provided by the catapult.
{... and many more, see FGFDM.cpp ...} {... and many more, see FGFDM.cpp ...}
invert: Negate the value of the property before setting on invert: Negate the value of the property before setting on
the object. the object.
@ -790,7 +793,7 @@ rotor: A rotor. Used for simulating helicopters. You can have one, two
head around the y-axis (TILTPITCH), the x-axis (TILTROLL) and the head around the y-axis (TILTPITCH), the x-axis (TILTROLL) and the
z-axis (TILTYAW). ROTORBALANCE is a factor for the balance. z-axis (TILTYAW). ROTORBALANCE is a factor for the balance.
rotorgear: If you are using one ore more rotors you have to define a rotorgear: If you are using one or more rotors you have to define a
rotorgear. It connects all the rotors and adds a simple engine. rotorgear. It connects all the rotors and adds a simple engine.
In future it will be possible, to add a YASim-engine. In future it will be possible, to add a YASim-engine.
max-power-engine: the maximum power of the engine, in kW. max-power-engine: the maximum power of the engine, in kW.
@ -805,31 +808,31 @@ rotorgear: If you are using one ore more rotors you have to define a
maximum acceleration rate of the engine in %/s, maximum acceleration rate of the engine in %/s,
default is 5%/s. default is 5%/s.
max-power-rotor-brake: the maximum power of the rotor brake, in kW max-power-rotor-brake: the maximum power of the rotor brake, in kW
at normal rpm (most? real rotor breaks would be overheated at normal rpm (most? real rotor brakes would be overheated
if used at normal rpm, but this is not simulated now) if used at normal rpm, but this is not simulated now)
rotorgear-friction: the power loss due to friction in kW at normal rotorgear-friction: the power loss due to friction in kW at normal
RPM RPM
yasimdragfactor: yasimdragfactor:
yasimliftfactor: the solver is not working with rotor-aircrafts. yasimliftfactor: the solver is not working with rotor-aircraft.
Therefore you have to specify the results yourself. Therefore you have to specify the results yourself.
10 for drag and 140 for lift seem to be good starting 10 for drag and 140 for lift seem to be good starting
values. Although the solve is not invoked for aircrafts values. Although the solve is not invoked for aircraft
with at least one rotor, you need to specify the cruise with at least one rotor, you need to specify the cruise
and the approach settings. The approach speed is needed to and the approach settings. The approach speed is needed to
calculate the gear springs. Use a speed of approx. 50knots. calculate the gear springs. Use a speed of approx. 50knots.
They do not need to match any real value. They do not need to match any real value.
The rotorgear needs a <control> subelement for the engine The rotorgear needs a <control> subelement for the engine
(ROTORGEARENGINEON) and can have furhter <control> subelements: (ROTORGEARENGINEON) and can have further <control> subelements:
ROTORBRAKE: rotor brake ROTORBRAKE: rotor brake
ROTORRELTARGET: the target rpm of the engine relative to ROTORRELTARGET: the target rpm of the engine relative to
the "normal" value for the governor. Default is the "normal" value for the governor. Default is
1. 1.
ROTORENGINEMAXRELTORQUE: the maximum torque of the engine ROTORENGINEMAXRELTORQUE: the maximum torque of the engine
relativ to the torque defined by the engine- relative to the torque defined by the engine-
power. Default is 1. By setting the rel-target power. Default is 1. By setting the rel-target
to a large number you get control over the to a large number you get control over the
engine by this control. engine by this control.
Alternativ you can use these two values for Alternatively you can use these two values for
individual start-up sequences (see the s58) individual start-up sequences (see the s58)