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Changing Syntax for 1.0 compatibility
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atmosphereScaleHeight to atmosphereDepth
maxAtmosphereAltitude to atmosphereDepth

velocityCurve got shortened to velCurve

atmosphereCurve got shortened to atmCurve

Some code from sswelm,
but was a little more rigorous.
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@Neouni
Neouni committed May 18, 2015
1 parent 649905d commit 5bf25dd
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Showing 28 changed files with 575 additions and 517 deletions.
919 changes: 460 additions & 459 deletions FNPlugin/AlcubierreDrive.cs
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Large diffs are not rendered by default.

3 changes: 2 additions & 1 deletion FNPlugin/ElectricEngineControllerFX.cs
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Original file line number Diff line number Diff line change
Expand Up @@ -320,7 +320,8 @@ protected void updateISP()
{
FloatCurve newISP = new FloatCurve();
newISP.Add(0, (float)(baseISP * _current_propellant.IspMultiplier));
_attached_engine.atmosphereCurve = newISP;
//_attached_engine.atmosphereCurve = newISP;
_attached_engine.atmCurve = newISP;
}

protected void updatePropellantBar()
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3 changes: 2 additions & 1 deletion FNPlugin/ElectricRCSController.cs
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Original file line number Diff line number Diff line change
Expand Up @@ -45,7 +45,8 @@ public void FixedUpdate() {
if (attachedRCS != null && HighLogic.LoadedSceneIsFlight && vessel.ActionGroups[KSPActionGroup.RCS]) {
double total_thrust = attachedRCS.thrustForces.Sum(frc => frc);
float curve_eval_point = (float)Math.Min(FlightGlobals.getStaticPressure(vessel.transform.position), 1.0);
double currentIsp = attachedRCS.atmosphereCurve.Evaluate(curve_eval_point);
//double currentIsp = attachedRCS.atmosphereCurve.Evaluate(curve_eval_point);
double currentIsp = attachedRCS.atmCurve.Evaluate(curve_eval_point);

double power_required = total_thrust * currentIsp * 9.82 * 0.5 / 1000.0;
double power_received = consumeFNResource(power_required * TimeWarp.fixedDeltaTime, FNResourceManager.FNRESOURCE_MEGAJOULES) / TimeWarp.fixedDeltaTime;
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49 changes: 33 additions & 16 deletions FNPlugin/FNNozzleController.cs
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Original file line number Diff line number Diff line change
Expand Up @@ -315,7 +315,8 @@ public void updateIspEngineParams() {
minISP = maxISP * 0.4f;
newISP.Add(0, Mathf.Min(maxISP, 2997.13f), 0, 0);
newISP.Add(1, Mathf.Min(minISP, 2997.13f), 0, 0);
myAttachedEngine.useVelocityCurve = false;
//myAttachedEngine.useVelocityCurve = false;
myAttachedEngine.useVelCurve = false;
myAttachedEngine.useEngineResponseTime = false;
} else {
if (myAttachedReactor.shouldScaleDownJetISP ()) {
Expand All @@ -332,13 +333,16 @@ public void updateIspEngineParams() {
vCurve.Add((float)(maxISP*g0*1.0/3.0), 1.0f);
vCurve.Add((float)(maxISP*g0), 1.0f);
vCurve.Add ((float)(maxISP*g0*4.0/3.0), 0);
myAttachedEngine.useVelocityCurve = true;
//myAttachedEngine.useVelocityCurve = true;
myAttachedEngine.useVelCurve = true;
myAttachedEngine.useEngineResponseTime = true;
myAttachedEngine.ignitionThreshold = 0.01f;
}

myAttachedEngine.atmosphereCurve = newISP;
myAttachedEngine.velocityCurve = vCurve;
//myAttachedEngine.atmosphereCurve = newISP;
myAttachedEngine.atmCurve = newISP;
//myAttachedEngine.velocityCurve = vCurve;
myAttachedEngine.velCurve = vCurve;
assThermalPower = myAttachedReactor.MaximumPower;
if (myAttachedReactor is InterstellarFusionReactor) {
assThermalPower = assThermalPower * 0.95f;
Expand Down Expand Up @@ -375,7 +379,8 @@ public bool hasStarted() {

public void estimateEditorPerformance() {
bool attached_reactor_upgraded = false;
FloatCurve atmospherecurve = new FloatCurve();
//FloatCurve atmospherecurve = new FloatCurve();
FloatCurve atmcurve = new FloatCurve();
float thrust = 0;
if (myAttachedReactor != null) {
if (myAttachedReactor is IUpgradeableModule) {
Expand All @@ -386,15 +391,20 @@ public void estimateEditorPerformance() {
}
maxISP = (float)(Math.Sqrt((double)myAttachedReactor.CoreTemperature) * isp_temp_rat * ispMultiplier);
minISP = maxISP * 0.4f;
atmospherecurve.Add(0, maxISP, 0, 0);
atmospherecurve.Add(1, minISP, 0, 0);
//atmospherecurve.Add(0, maxISP, 0, 0);
//atmospherecurve.Add(1, minISP, 0, 0);
atmcurve.Add(0, maxISP, 0, 0);
atmcurve.Add(1, minISP, 0, 0);
thrust = (float)(2 * myAttachedReactor.MaximumPower * 1000 / g0 / maxISP);
myAttachedEngine.maxThrust = thrust;
myAttachedEngine.atmosphereCurve = atmospherecurve;
//myAttachedEngine.atmosphereCurve = atmospherecurve;
myAttachedEngine.atmCurve = atmcurve;
} else {
atmospherecurve.Add(0, 0.00001f, 0, 0);
//atmospherecurve.Add(0, 0.00001f, 0, 0);
atmcurve.Add(0, 0.00001f, 0, 0);
myAttachedEngine.maxThrust = thrust;
myAttachedEngine.atmosphereCurve = atmospherecurve;
//myAttachedEngine.atmosphereCurve = atmospherecurve;
myAttachedEngine.atmCurve = atmcurve;
}
}

Expand All @@ -405,7 +415,8 @@ public override void OnFixedUpdate() {
}
updateIspEngineParams ();
float curve_eval_point = (float)Math.Min (FlightGlobals.getStaticPressure (vessel.transform.position), 1.0);
float currentIsp = myAttachedEngine.atmosphereCurve.Evaluate (curve_eval_point);
//float currentIsp = myAttachedEngine.atmosphereCurve.Evaluate (curve_eval_point);
float currentIsp = myAttachedEngine.atmCurve.Evaluate (curve_eval_point);
double ispratio = currentIsp / maxISP;
this.current_isp = currentIsp;
// scale down thrust if it's attached to the wrong sized reactor
Expand Down Expand Up @@ -460,7 +471,9 @@ public override void OnFixedUpdate() {
//double additional_thrust_compensator = myAttachedEngine.finalThrust / (myAttachedEngine.maxThrust * myAttachedEngine.currentThrottle)/ispratio;
double engine_thrust = engineMaxThrust/myAttachedEngine.thrustPercentage*100;
// engine thrust fixed
//print ("A: " + engine_thrust*myAttachedEngine.velocityCurve.Evaluate((float)vessel.srf_velocity.magnitude));
//print ("A: " + //engine_thrust*myAttachedEngine.velocityCurve.Evaluate((float)vessel.srf_velocity.magnitude));
if (!double.IsInfinity(engine_thrust) && !double.IsNaN(engine_thrust)) {
engine_thrust*myAttachedEngine.veloCurve.Evaluate((float)vessel.srf_velocity.magnitude));
if (!double.IsInfinity(engine_thrust) && !double.IsNaN(engine_thrust)) {
if (isLFO) {
myAttachedEngine.maxThrust = (float)(2.2222 * engine_thrust);
Expand All @@ -475,8 +488,10 @@ public override void OnFixedUpdate() {
if (current_isp > 0) {
double vcurve_at_current_velocity = 1;

if (myAttachedEngine.useVelocityCurve && myAttachedEngine.velocityCurve != null) {
vcurve_at_current_velocity = myAttachedEngine.velocityCurve.Evaluate((float)vessel.srf_velocity.magnitude);
//if (myAttachedEngine.useVelocityCurve && myAttachedEngine.velocityCurve != null) {
//vcurve_at_current_velocity = myAttachedEngine.velocityCurve.Evaluate((float)vessel.srf_velocity.magnitude);
if (myAttachedEngine.useVelCurve && myAttachedEngine.velCurve != null) {
vcurve_at_current_velocity = myAttachedEngine.velCurve.Evaluate((float)vessel.srf_velocity.magnitude);
}
//if (!double.IsNaN(additional_thrust_compensator) && !double.IsInfinity(additional_thrust_compensator)) {
//vcurve_at_current_velocity = additional_thrust_compensator;
Expand All @@ -495,8 +510,10 @@ public override void OnFixedUpdate() {
if (myAttachedEngine.realIsp > 0) {
atmospheric_limit = getAtmosphericLimit();
double vcurve_at_current_velocity = 1;
if (myAttachedEngine.useVelocityCurve) {
vcurve_at_current_velocity = myAttachedEngine.velocityCurve.Evaluate((float)vessel.srf_velocity.magnitude);
//if (myAttachedEngine.useVelocityCurve) {
//vcurve_at_current_velocity = myAttachedEngine.velocityCurve.Evaluate((float)vessel.srf_velocity.magnitude);
if (myAttachedEngine.useVelCurve) {
vcurve_at_current_velocity = myAttachedEngine.velCurve.Evaluate((float)vessel.srf_velocity.magnitude);
}
fuel_flow_rate = myAttachedEngine.maxThrust / myAttachedEngine.realIsp / g0 / 0.005 * TimeWarp.fixedDeltaTime;
if (vcurve_at_current_velocity > 0 && !double.IsInfinity(vcurve_at_current_velocity) && !double.IsNaN(vcurve_at_current_velocity)) {
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27 changes: 18 additions & 9 deletions FNPlugin/FNNozzleControllerFX.cs
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Original file line number Diff line number Diff line change
Expand Up @@ -280,7 +280,8 @@ public void updateIspEngineParams() {
minISP = maxISP * 0.4f;
newISP.Add (0, Mathf.Min(maxISP, 2997.13f), 0, 0);
newISP.Add(1, Mathf.Min(minISP, 2997.13f), 0, 0);
myAttachedEngine.useVelocityCurve = false;
//myAttachedEngine.useVelocityCurve = false;
myAttachedEngine.useVelCurve = false;
myAttachedEngine.useEngineResponseTime = false;
} else {
if (myAttachedReactor.shouldScaleDownJetISP ()) {
Expand All @@ -297,13 +298,16 @@ public void updateIspEngineParams() {
vCurve.Add((float)(maxISP*g0*1.0/3.0), 0.9f);
vCurve.Add((float)(maxISP*g0), 1.0f);
vCurve.Add ((float)(maxISP*g0*4.0/3.0), 0);
myAttachedEngine.useVelocityCurve = true;
//myAttachedEngine.useVelocityCurve = true;
myAttachedEngine.useVelCurve = true;
myAttachedEngine.useEngineResponseTime = true;
myAttachedEngine.ignitionThreshold = 0.01f;
}

myAttachedEngine.atmosphereCurve = newISP;
myAttachedEngine.velocityCurve = vCurve;
//myAttachedEngine.atmosphereCurve = newISP;
myAttachedEngine.atmCurve = newISP;
//myAttachedEngine.velocityCurve = vCurve;
myAttachedEngine.velCurve = vCurve;
assThermalPower = myAttachedReactor.MaximumPower;
}

Expand Down Expand Up @@ -342,7 +346,8 @@ public override void OnFixedUpdate() {
}
updateIspEngineParams ();
float curve_eval_point = (float)Math.Min (FlightGlobals.getStaticPressure (vessel.transform.position), 1.0);
float currentIsp = myAttachedEngine.atmosphereCurve.Evaluate (curve_eval_point);
//float currentIsp = myAttachedEngine.atmosphereCurve.Evaluate (curve_eval_point);
float currentIsp = myAttachedEngine.atmCurve.Evaluate (curve_eval_point);
double ispratio = currentIsp / maxISP;
this.current_isp = currentIsp;
// scale down thrust if it's attached to the wrong sized reactor
Expand Down Expand Up @@ -404,8 +409,10 @@ public override void OnFixedUpdate() {
// amount of fuel being used at max throttle with no atmospheric limits
if (current_isp > 0) {
double vcurve_at_current_velocity = 1;
if (myAttachedEngine.useVelocityCurve) {
vcurve_at_current_velocity = myAttachedEngine.velocityCurve.Evaluate((float)vessel.srf_velocity.magnitude);
//if (myAttachedEngine.useVelocityCurve) {
if (myAttachedEngine.useVelCurve) {
//vcurve_at_current_velocity = myAttachedEngine.velocityCurve.Evaluate((float)vessel.srf_velocity.magnitude);
vcurve_at_current_velocity = myAttachedEngine.velCurve.Evaluate((float)vessel.srf_velocity.magnitude);
}
fuel_flow_rate = engine_thrust / current_isp / g0 / 0.005 * TimeWarp.fixedDeltaTime;
if (vcurve_at_current_velocity > 0) {
Expand All @@ -417,8 +424,10 @@ public override void OnFixedUpdate() {
if (myAttachedEngine.realIsp > 0) {
atmospheric_limit = getAtmosphericLimit();
double vcurve_at_current_velocity = 1;
if (myAttachedEngine.useVelocityCurve) {
vcurve_at_current_velocity = myAttachedEngine.velocityCurve.Evaluate((float)vessel.srf_velocity.magnitude);
//if (myAttachedEngine.useVelocityCurve) {
if (myAttachedEngine.useVelCurve) {
//vcurve_at_current_velocity = myAttachedEngine.velocityCurve.Evaluate((float)vessel.srf_velocity.magnitude);
vcurve_at_current_velocity = myAttachedEngine.velCurve.Evaluate((float)vessel.srf_velocity.magnitude);
}
fuel_flow_rate = myAttachedEngine.maxThrust / myAttachedEngine.realIsp / g0 / 0.005 * TimeWarp.fixedDeltaTime/vcurve_at_current_velocity;
}else {
Expand Down
7 changes: 4 additions & 3 deletions FNPlugin/FNRadiator.cs
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Original file line number Diff line number Diff line change
Expand Up @@ -293,14 +293,15 @@ public override void OnUpdate() {
}

public override void OnFixedUpdate() {
float atmosphere_height = vessel.mainBody.maxAtmosphereAltitude;
//float atmosphere_height = vessel.mainBody.maxAtmosphereAltitude;
float atmosphere_height = (float)vessel.mainBody.atmosphereDepth;
float vessel_height = (float) vessel.mainBody.GetAltitude (vessel.transform.position);
float conv_power_dissip = 0;
if (vessel.altitude <= PluginHelper.getMaxAtmosphericAltitude(vessel.mainBody)) {
float pressure = (float) FlightGlobals.getStaticPressure (vessel.transform.position);
float dynamic_pressure = (float) (0.5*pressure*1.2041*vessel.srf_velocity.sqrMagnitude);
pressure += dynamic_pressure;
float low_temp = FlightGlobals.getExternalTemperature (vessel.transform.position);
float low_temp = (float) FlightGlobals.getExternalTemperature (vessel.transform.position);

float delta_temp = Mathf.Max(0, (float)current_rad_temp - low_temp);
conv_power_dissip = pressure * delta_temp * radiatorArea * rad_const_h/1e6f * TimeWarp.fixedDeltaTime*convectiveBonus;
Expand Down Expand Up @@ -432,7 +433,7 @@ private void colorHeat()
{
const String KSPShader = "KSP/Emissive/Bumped Specular";
float currentTemperature = getRadiatorTemperature();
float maxTemperature = part.maxTemp;
float maxTemperature = (float) part.maxTemp;

double temperatureRatio = currentTemperature / maxTemperature;
Color emissiveColor = new Color((float)(Math.Pow(temperatureRatio, 3)), 0.0f, 0.0f, 1.0f);
Expand Down
3 changes: 2 additions & 1 deletion FNPlugin/InterstellarMagneticNozzleControllerFX.cs
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Original file line number Diff line number Diff line change
Expand Up @@ -53,7 +53,8 @@ public void FixedUpdate() {
double isp = Math.Sqrt(joules_per_amu * 2.0 / GameConstants.ATOMIC_MASS_UNIT) / GameConstants.STANDARD_GRAVITY;
FloatCurve new_isp = new FloatCurve();
new_isp.Add(0, (float)isp, 0, 0);
_attached_engine.atmosphereCurve = new_isp;
//_attached_engine.atmosphereCurve = new_isp;
_attached_engine.atmCurve = new_isp;

double charged_power_received = consumeFNResource(max_power * TimeWarp.fixedDeltaTime * _attached_engine.currentThrottle, FNResourceManager.FNRESOURCE_CHARGED_PARTICLES) / TimeWarp.fixedDeltaTime;
consumeFNResource(charged_power_received * TimeWarp.fixedDeltaTime, FNResourceManager.FNRESOURCE_WASTEHEAT);
Expand Down
6 changes: 4 additions & 2 deletions FNPlugin/ModuleSabreHeating.cs
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Original file line number Diff line number Diff line change
Expand Up @@ -52,7 +52,8 @@ public void FixedUpdate() {

if (rapier_engine != null)
{
if (rapier_engine.isOperational && rapier_engine.currentThrottle > 0 && rapier_engine.useVelocityCurve)
//if (rapier_engine.isOperational && rapier_engine.currentThrottle > 0 && rapier_engine.useVelocityCurve)
if (rapier_engine.isOperational && rapier_engine.currentThrottle > 0 && rapier_engine.useVelCurve)
{
float temp = (float)Math.Max((Math.Sqrt(vessel.srf_velocity.magnitude) * 20.0 / GameConstants.atmospheric_non_precooled_limit) * part.maxTemp * proportion, 1);
if (temp >= (part.maxTemp - 10.0f))
Expand All @@ -71,7 +72,8 @@ public void FixedUpdate() {

if (rapier_engine2 != null)
{
if (rapier_engine2.isOperational && rapier_engine2.currentThrottle > 0 && rapier_engine2.useVelocityCurve)
//if (rapier_engine2.isOperational && rapier_engine2.currentThrottle > 0 && rapier_engine2.useVelocityCurve)
if (rapier_engine2.isOperational && rapier_engine2.currentThrottle > 0 && rapier_engine2.useVelCurve)
{
float temp = (float)Math.Max((Math.Sqrt(vessel.srf_velocity.magnitude) * 20.0 / GameConstants.atmospheric_non_precooled_limit) * part.maxTemp * proportion, 1);
if (temp >= (part.maxTemp - 10.0f))
Expand Down
3 changes: 2 additions & 1 deletion FNPlugin/PluginHelper.cs
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Original file line number Diff line number Diff line change
Expand Up @@ -249,7 +249,8 @@ public static float getMaxAtmosphericAltitude(CelestialBody body)
{
return 0;
}
return (float)-body.atmosphereScaleHeight * 1000.0f * Mathf.Log(1e-6f);
//return (float)-body.atmosphereScaleHeight * 1000.0f * Mathf.Log(1e-6f);
return (float)-body.atmosphereDepth * 1000.0f * Mathf.Log(1e-6f);
}

public static float getScienceMultiplier(int refbody, bool landed)
Expand Down
6 changes: 4 additions & 2 deletions FNPlugin/VistaEngineController.cs
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Original file line number Diff line number Diff line change
Expand Up @@ -37,7 +37,8 @@ public override void OnStart(PartModule.StartState state) {
if (state == StartState.Editor) {return;}

ModuleEngines curEngineT = (ModuleEngines)this.part.Modules ["ModuleEngines"];
minISP = curEngineT.atmosphereCurve.Evaluate(0);
//minISP = curEngineT.atmosphereCurve.Evaluate(0);
minISP = curEngineT.atmCurve.Evaluate(0);

standard_deut_rate = curEngineT.propellants.FirstOrDefault(pr => pr.name == InterstellarResourcesConfiguration.Instance.Deuterium).ratio;
standard_lith_rate = curEngineT.propellants.FirstOrDefault(pr => pr.name == InterstellarResourcesConfiguration.Instance.Tritium).ratio;
Expand Down Expand Up @@ -140,7 +141,8 @@ public override void OnFixedUpdate() {
//curEngineT.propellants[2].ratio = (float)(standard_lith_rate / throttle / throttle);
FloatCurve newISP = new FloatCurve();
newISP.Add(0, (float)(minISP / throttle));
curEngineT.atmosphereCurve = newISP;
//curEngineT.atmosphereCurve = newISP;
curEngineT.atmCurve = newISP;
if (power >= 2500 * TimeWarp.fixedDeltaTime) {
curEngineT.maxThrust = 1100;
} else {
Expand Down
3 changes: 2 additions & 1 deletion GameData/WarpPlugin/Parts/Engines/AluminiumHybrid/part.cfg
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Original file line number Diff line number Diff line change
Expand Up @@ -89,7 +89,8 @@ MODULE
name = Oxidizer
ratio = 4.05
}
atmosphereCurve
//atmosphereCurve
atmCurve
{
key = 0 286
key = 1 250
Expand Down
3 changes: 2 additions & 1 deletion GameData/WarpPlugin/Parts/Engines/AugmentedArcjet/part0.cfg
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Original file line number Diff line number Diff line change
Expand Up @@ -142,7 +142,8 @@ MODULE
name = LiquidFuel
ratio = 1
}
atmosphereCurve
//atmosphereCurve
atmCurve
{
key = 0 2854
}
Expand Down
3 changes: 2 additions & 1 deletion GameData/WarpPlugin/Parts/Engines/AugmentedArcjet/part1.cfg
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Original file line number Diff line number Diff line change
Expand Up @@ -142,7 +142,8 @@ MODULE
name = LiquidFuel
ratio = 1
}
atmosphereCurve
//atmosphereCurve
atmCurve
{
key = 0 2854
}
Expand Down
3 changes: 2 additions & 1 deletion GameData/WarpPlugin/Parts/Engines/MPD/part0.cfg
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Original file line number Diff line number Diff line change
Expand Up @@ -139,7 +139,8 @@ MODULE
name = LiquidFuel
ratio = 1
}
atmosphereCurve
//atmosphereCurve
atmCurve
{
key = 0 11213
}
Expand Down
3 changes: 2 additions & 1 deletion GameData/WarpPlugin/Parts/Engines/MPD/part1.cfg
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Original file line number Diff line number Diff line change
Expand Up @@ -139,7 +139,8 @@ MODULE
name = LiquidFuel
ratio = 1
}
atmosphereCurve
//atmosphereCurve
atmCurve
{
key = 0 11213
}
Expand Down
3 changes: 2 additions & 1 deletion GameData/WarpPlugin/Parts/Engines/MPD/part2.cfg
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Original file line number Diff line number Diff line change
Expand Up @@ -139,7 +139,8 @@ MODULE
name = LiquidFuel
ratio = 1
}
atmosphereCurve
//atmosphereCurve
atmCurve
{
key = 0 11213
}
Expand Down
3 changes: 2 additions & 1 deletion GameData/WarpPlugin/Parts/Engines/MagneticNozzle/part1.cfg
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Original file line number Diff line number Diff line change
Expand Up @@ -105,7 +105,8 @@ MODULE
ratio = 1.0
DrawGauge = True
}
atmosphereCurve
//atmosphereCurve
atmCurve
{
key = 0 36000
key = 1 32000
Expand Down
3 changes: 2 additions & 1 deletion GameData/WarpPlugin/Parts/Engines/MagneticNozzle/part2.cfg
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Original file line number Diff line number Diff line change
Expand Up @@ -105,7 +105,8 @@ MODULE
ratio = 1.0
DrawGauge = True
}
atmosphereCurve
//atmosphereCurve
atmCurve
{
key = 0 36000
key = 1 32000
Expand Down
3 changes: 2 additions & 1 deletion GameData/WarpPlugin/Parts/Engines/MagneticNozzle/part3.cfg
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Original file line number Diff line number Diff line change
Expand Up @@ -105,7 +105,8 @@ MODULE
ratio = 1.0
DrawGauge = True
}
atmosphereCurve
//atmosphereCurve
atmCurve
{
key = 0 36000
key = 1 32000
Expand Down
3 changes: 2 additions & 1 deletion GameData/WarpPlugin/Parts/Engines/MethaneEngine/part.cfg
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Original file line number Diff line number Diff line change
Expand Up @@ -78,7 +78,8 @@ MODULE
name = Oxidizer
ratio = 1
}
atmosphereCurve
//atmosphereCurve
atmCurve
{
key = 0 368
key = 1 309
Expand Down
3 changes: 2 additions & 1 deletion GameData/WarpPlugin/Parts/Engines/ThermalRocketNozzle/part0.cfg
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Original file line number Diff line number Diff line change
Expand Up @@ -79,7 +79,8 @@ MODULE
name = Oxidizer
ratio = 1.1
}
atmosphereCurve
//atmosphereCurve
atmCurve
{
key = 0 1000
key = 1 400
Expand Down
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