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feat(flight): enhance flight model with transonic drag and vortex lift features

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richard committed 2026-10-28 23:14:37 +01:00
1 parent 599ecae21f
commit 44a5f7f9bc
12 files changed
+177 -26
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src/main/java/dev/lumareth/improvedAerodynamics/flight/AeroState.java
+4 -7
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@@ -205,10 +205,7 @@ public final class AeroState implements PhysicsBridge.Publishable {
private void evaluate(Frame frame, Vector3dc centerOfMass, double[] v, double[] w, boolean improved, boolean commit, Wrench out) {
out.clear();
double weight = clock.weight();
double liftConstant = ImprovedAero.LIFT_CONSTANT;
double stallAngleScale = Config.STALL_ANGLE_SCALE.get();
double liftScale = Config.LIFT_SCALE.get();
double thinDrag = Config.STABILIZER_DRAG.get();
ImprovedAero.Tuning tuning = improved ? ImprovedAero.Tuning.read() : null;
double[] r = new double[3];
if (commit) {
wingStalled = false;
@@ -227,7 +224,7 @@ public final class AeroState implements PhysicsBridge.Publishable {
double input = s.type().controllable ? input(s, node, state, 0.0) : 0.0;
if (improved) {
boolean nowStalled = ImprovedAero.evaluate(s, v, w, r, input, weight, liftConstant, liftScale, stallAngleScale, thinDrag, stalled[i], out);
boolean nowStalled = ImprovedAero.evaluate(s, v, w, r, input, weight, tuning, stalled[i], out);
if (commit) {
stalled[i] = nowStalled;
wingStalled |= nowStalled && s.type() == SurfaceType.WING;
@@ -242,7 +239,7 @@ public final class AeroState implements PhysicsBridge.Publishable {
probe.clear();
double base = 0.0;
if (improved) {
ImprovedAero.evaluate(s, v, w, r, input, weight, liftConstant, liftScale, stallAngleScale, thinDrag, stalled[i], probe);
ImprovedAero.evaluate(s, v, w, r, input, weight, tuning, stalled[i], probe);
} else {
WariumAero.evaluate(s, v, w, r, input, weight, probe);
}
@@ -250,7 +247,7 @@ public final class AeroState implements PhysicsBridge.Publishable {
probe.clear();
double nudged = input(s, node, state, delta);
if (improved) {
ImprovedAero.evaluate(s, v, w, r, nudged, weight, liftConstant, liftScale, stallAngleScale, thinDrag, stalled[i], probe);
ImprovedAero.evaluate(s, v, w, r, nudged, weight, tuning, stalled[i], probe);
} else {
WariumAero.evaluate(s, v, w, r, nudged, weight, probe);
}