Difference between revisions of "Parts/Aero/airplaneFins/standardCanard.cfg"

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<pre>
+
{{Part config|Standard Canard|2=PART
// this is a sample config file, for determining a good file format for defining part parameters
+
{
// comment line - ignored by cfg parser
+
name = CanardController
// empty lines, or lines without a '=' sign are also ignored
+
module = Part
// all other lines are split at the '=' sign, and the left operand is used to know what parameter we are setting
+
author = C. Jenkins, Porkjet
// diferent parameters require data in different formats (see docs), and each module has it's own parameters (again, see docs)
+
rescaleFactor = 1
// each assignment must be in a single line. Lines without assignments will be ignored. (You CAN turn on word wrap, though)
+
node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1
// each keyword here relates to an existing variable in the assigned module. If the keyword isn't found, it is ignored.
+
CoMOffset = -0.55, -0.15, 0
// conversely, if a keyword is left unassigned (as in not in the file), it will be initialized with it's default value
+
CoLOffset = -0.55, -0.15, 0
// This is done automatically, so any public variable defined in the loaded module can be accessed this way (provided it's value can be parsed)
+
CoPOffset = -0.55, -0.15, 0
 
+
TechRequired = advAerodynamics
 
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entryCost = 11400
// --- general parameters ---
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cost = 720
name = CanardController
+
category = Aero
module = ControlSurface
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subcategory = 0
author = C. Jenkins
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title = #autoLOC_500130 //#autoLOC_500130 = Standard Canard
 
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manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division
// --- asset parameters ---
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description = #autoLOC_500131 //#autoLOC_500131 = Our engineers had a stroke of inspiration after "visiting" the Kerlington production facilities. Introducing our new controllable canards. Warning, hard maneuvering may cause unintended stage separation.
mesh = model.mu
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attachRules = 0,1,0,1,0
scale = 0.1
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mass = 0.1
 
+
thermalMassModifier = 8.0
 
+
// heatConductivity = 0.06 // half default
// --- editor parameters ---
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emissiveConstant = 0.95
cost = 500
+
dragModelType = none
category = Aero
+
maximum_drag = 0.02
subcategory = 0
+
minimum_drag = 0.02
title = Standard Canard
+
angularDrag = 3
manufacturer = c7 Aerospace
+
crashTolerance = 12
description = Our engineers had a stroke of inspiration after "visiting" the kerlington production facilities. Introducing our new controllable canards. Warning, hard manuvering may cause unintended stage separation.
+
maxTemp = 2400
// attachment rules: stack, srfAttach, allowStack, allowSrfAttach, allowCollision
+
explosionPotential = 0.1
attachRules = 0,1,0,1,0
+
fuelCrossFeed = True
 
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bulkheadProfiles = srf
// --- node definitions ---
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tags = #autoLOC_500132 //#autoLOC_500132 = aero (air control (elev fligh (fore lift plane )rudder stab swept tail
// definition format is Position X, Position Y, Position Z, Up X, Up Y, Up Z
+
MODEL
node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0
+
{
 
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model = Squad/Parts/Aero/airplaneFins/Canard
 
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}
// --- standard part parameters ---
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MODULE
mass = 0.04
+
{
dragModelType = override
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name = ModuleControlSurface
maximum_drag = 0.02
+
useInternalDragModel = True
minimum_drag = 0.02
+
dragCoeff = 0.5
angularDrag = 3
+
deflectionLiftCoeff = 0.52 //1.83m^2
crashTolerance = 12
+
ctrlSurfaceRange = 15
maxTemp = 3400
+
ctrlSurfaceArea = 1
explosionPotential = 0.1
+
actuatorSpeed = 30
fuelCrossFeed = True
+
transformName = ctrlSrf
 
+
}
// --- winglet parameters ---
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MODULE
// dragCoeff will override the maximum_drag value
+
{
dragCoeff = 0.5
+
name = ModuleCargoPart
deflectionLiftCoeff = 0.7
+
packedVolume = -1
ctrlSurfaceRange = 20
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}
ctrlSurfaceArea = 0.95
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}
 
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}}
 
 
// --- tweakables (coming soon...) ---
 
 
 
 
 
 
 
 
 
// ----- DO NOT EDIT BELOW THIS POINT ------
 
</pre>
 

Latest revision as of 10:59, 13 October 2024

This is the configuration file for Standard Canard.
PART
{
	name = CanardController
	module = Part
	author = C. Jenkins, Porkjet
	rescaleFactor = 1
	node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1
	CoMOffset = -0.55, -0.15, 0
	CoLOffset = -0.55, -0.15, 0
	CoPOffset = -0.55, -0.15, 0
	TechRequired = advAerodynamics
	entryCost = 11400
	cost = 720
	category = Aero
	subcategory = 0
	title = #autoLOC_500130 //#autoLOC_500130 = Standard Canard
	manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division
	description = #autoLOC_500131 //#autoLOC_500131 = Our engineers had a stroke of inspiration after "visiting" the Kerlington production facilities. Introducing our new controllable canards. Warning, hard maneuvering may cause unintended stage separation.
	attachRules = 0,1,0,1,0
	mass = 0.1
	thermalMassModifier = 8.0
	// heatConductivity = 0.06 // half default
	emissiveConstant = 0.95
	dragModelType = none
	maximum_drag = 0.02
	minimum_drag = 0.02
	angularDrag = 3
	crashTolerance = 12
	maxTemp = 2400
	explosionPotential = 0.1
	fuelCrossFeed = True
	bulkheadProfiles = srf
	tags = #autoLOC_500132 //#autoLOC_500132 = aero (air control (elev fligh (fore lift plane )rudder stab swept tail
	MODEL
	{
		model = Squad/Parts/Aero/airplaneFins/Canard
	}
	MODULE
	{
		name = ModuleControlSurface
		useInternalDragModel = True
		dragCoeff = 0.5
		deflectionLiftCoeff = 0.52		//1.83m^2
		ctrlSurfaceRange = 15
		ctrlSurfaceArea = 1
		actuatorSpeed = 30
		transformName = ctrlSrf
	}
	MODULE
	{
		name = ModuleCargoPart		
		packedVolume = -1
	}
}