internal override void Display()
{
if (IsActive && ImGui.Begin("Ordnance Design"))
{
ImGui.Combo("Current Designs", ref _payloadSelectedIndex, _currentDesignNames, _currentDesignNames.Length);
ImGui.NewLine();
BorderGroup.BeginBorder("Payload:");
if (ImGui.Combo("Payload type", ref _payloadSelectedIndex, _payload, _payload.Length))
{
//_selectedPayload = _payloadTypes[_payloadSelectedIndex].GetAttribute<OrdnancePayloadAtb>();
_selectedComponentDesigns[_payloadTypes[_payloadSelectedIndex]] = _payloadCount;
RefreshMass();
}
if (ImGui.SliderInt("Payload Count", ref _payloadCount, 1, 100))
{
_selectedComponentDesigns[_payloadTypes[_payloadSelectedIndex]] = _payloadCount;
RefreshMass();
}
var whmass = _payloadTypes[_payloadSelectedIndex].Mass * _payloadCount;
ImGui.Text("Mass: " + Stringify.Mass(whmass));
//ImGui.Text("Payload Trigger Type: " + _selectedPayload.Trigger);
BorderGroup.EndBoarder();
ImGui.NewLine();
BorderGroup.BeginBorder("Electronics Suite:");
if (ImGui.Combo("ElectronicsSuite", ref _electronicsSelectedIndex, _electronicsPackage, _electronicsPackage.Length))
{
_selectedComponentDesigns[_eleccPackTypes[_electronicsSelectedIndex]] = 1;
RefreshMass();
}
var mass = _eleccPackTypes[_electronicsSelectedIndex].Mass;
ImGui.Text("Mass: " + Stringify.Mass(mass));
BorderGroup.EndBoarder();
ImGui.NewLine();
BorderGroup.BeginBorder("Engine:");
if (ImGui.Combo("Engine Designs", ref _engineSelectedIndex, _engineDesigns, _engineDesigns.Length))
{
ComponentDesign engineDesign = _engineTypes[_engineSelectedIndex];
_selectedComponentDesigns[engineDesign] = _engineCount;
RefreshMass();
}
if (ImGui.SliderInt("Engine Count", ref _engineCount, 1, 256))
{
_selectedComponentDesigns[_engineTypes[_engineSelectedIndex]] = _engineCount;
RefreshMass();
}
var emass = _engineTypes[_engineSelectedIndex].Mass * _engineCount;
ImGui.Text("Mass: " + Stringify.Mass(emass));
BorderGroup.EndBoarder();
ImGui.NewLine();
ImGui.Text("Total Mass: " + Stringify.Mass(_totalMass));
var enginedesign = _engineTypes[_engineSelectedIndex];
var atb = enginedesign.GetAttribute <NewtonionThrustAtb>();
double burnRate = atb.FuelBurnRate * _engineCount;
double exaustVel = atb.ExhaustVelocity;
double thrustNewtons = burnRate * exaustVel;
double burnTime = _fuelKG / burnRate;
double dv = OrbitMath.TsiolkovskyRocketEquation(_totalMass, _totalMass - _fuelKG, exaustVel);
ImGui.Text("Burn Time: " + burnTime + "s");
ImGui.Text("Thrust: " + Stringify.Thrust(thrustNewtons));
ImGui.Text("DeltaV: " + Stringify.Velocity(dv));
ImGui.InputText("Design Name", _designName, (uint)_designName.Length);
NewDesignButton();
}
}
internal override void Display()
{
if (IsActive && ImGui.Begin("Ordnance Design"))
{
ImGui.Combo("Current Designs", ref _payloadSelectedIndex, _currentDesignNames, _currentDesignNames.Length);
ImGui.NewLine();
BorderGroup.Begin("Payload:");
if (ImGui.Combo("Payload type", ref _payloadSelectedIndex, _payload, _payload.Length))
{
//_selectedPayload = _payloadTypes[_payloadSelectedIndex].GetAttribute<OrdnancePayloadAtb>();
_selectedComponentDesigns[_payloadTypes[_payloadSelectedIndex]] = _payloadCount;
RefreshMass();
}
if (ImGui.SliderInt("Payload Count", ref _payloadCount, 1, 100))
{
_selectedComponentDesigns[_payloadTypes[_payloadSelectedIndex]] = _payloadCount;
RefreshMass();
}
var whmass = _payloadTypes[_payloadSelectedIndex].MassPerUnit * _payloadCount;
ImGui.Text("Mass: " + Stringify.Mass(whmass));
//ImGui.Text("Payload Trigger Type: " + _selectedPayload.Trigger);
BorderGroup.End();
ImGui.NewLine();
BorderGroup.Begin("Electronics Suite:");
if (ImGui.Combo("ElectronicsSuite", ref _electronicsSelectedIndex, _electronicsPackage, _electronicsPackage.Length))
{
_selectedComponentDesigns[_eleccPackTypes[_electronicsSelectedIndex]] = 1;
RefreshMass();
}
var mass = _eleccPackTypes[_electronicsSelectedIndex].MassPerUnit;
ImGui.Text("Mass: " + Stringify.Mass(mass));
BorderGroup.End();
ImGui.NewLine();
BorderGroup.Begin("Engine:");
if (ImGui.Combo("Engine Types", ref _engineDesignTypeIndex, _engineTypeNames, _engineTypeNames.Length))
{
_engineDesigner = new ComponentDesigner(_engineTemplates[_engineDesignTypeIndex], _factionTech);
_engineDesigner.SetAttributes();
}
if (_engineDesigner != null)
{
PartDesignUI.GuiDesignUI(_engineDesigner);
_thrusterSizeKG = _engineDesigner.MassValue;
RefreshMass();
}
if (ImGui.SliderFloat("Fuel", ref _fuelKG, 1, 1000))
{
RefreshMass();
}
BorderGroup.End();
ImGui.NewLine();
ImGui.Text("Total Mass: " + Stringify.Mass(_totalMass));
double burnRate = 0;
double exaustVel = 0;
if (_engineDesigner != null)
{
var atb = _engineDesigner.GetAttribute <NewtonionThrustAtb>();
burnRate = atb.FuelBurnRate;
exaustVel = atb.ExhaustVelocity;
}
double thrustNewtons = burnRate * exaustVel;
double burnTime = _fuelKG / burnRate;
double dv = OrbitMath.TsiolkovskyRocketEquation(_totalMass, _totalMass - _fuelKG, exaustVel);
ImGui.Text("Burn Time: " + burnTime + "s");
ImGui.Text("Thrust: " + Stringify.Thrust(thrustNewtons));
ImGui.Text("Acceleration (wet): " + Stringify.Velocity(thrustNewtons / _totalMass));
ImGui.Text("Acceleration (dry): " + Stringify.Velocity(thrustNewtons / (_totalMass - _fuelKG)));
ImGui.Text("DeltaV: " + Stringify.Velocity(dv));
ImGui.InputText("Design Name", _designName, (uint)_designName.Length);
NewDesignButton();
}
}
