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authorhybrid <hybrid@hybridlabs.pro>2026-07-12 21:30:48 +0300
committerhybrid <hybrid@hybridlabs.pro>2026-07-12 21:30:48 +0300
commit4020a7124a80a608acd41a913ca5f6ad3ff3d488 (patch)
tree53ecefe6279497a4d2c6a921cab6dade6ed85e40 /src
parent866393b70f5baddcaf9571b7240ebd4ce44bc67c (diff)
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add: tmp commit
Diffstat (limited to '')
-rw-r--r--src/atragmx.c14
-rw-r--r--src/ballistics.c31
2 files changed, 42 insertions, 3 deletions
diff --git a/src/atragmx.c b/src/atragmx.c
index af68b2c..ff684c3 100644
--- a/src/atragmx.c
+++ b/src/atragmx.c
@@ -97,8 +97,7 @@ ATragMXSolution *ATragMXCalcSolution(ATragMXContext *ctx, ace_config *ace) {
if (ace->ballistics->enabled)
ctx->gun.ballistic_coef
- = atmospheric_correction(
- ctx->gun.ballistic_coef,
+ = atmospheric_correction(ctx->gun.ballistic_coef,
ctx->atmosphere.temperature,
ctx->atmosphere.barometric_pressure,
ctx->atmosphere.relative_humidity,
@@ -129,8 +128,17 @@ ATragMXSolution *ATragMXCalcSolution(ATragMXContext *ctx, ace_config *ace) {
// calculate magnitude of bullet.velocity
bullet.speed = hypot(bullet.velocity[0],
hypot(bullet.velocity[1], bullet.velocity[2]));
+ memcpy(local_solution.true_velocity,
+ (double[3]){bullet.velocity[0] - wind1[0],
+ bullet.velocity[1] - wind1[1],
+ bullet.velocity[2] - wind1[2]},
+ sizeof(local_solution.true_velocity));
+ local_solution.true_speed = hypot(local_solution.true_velocity[0],
+ hypot(local_solution.true_velocity[1],
+ local_solution.true_velocity[2]));
+
+ if (ace->ballistics->enabled)
-
}
return sln;
diff --git a/src/ballistics.c b/src/ballistics.c
index 10d97da..418318a 100644
--- a/src/ballistics.c
+++ b/src/ballistics.c
@@ -4,6 +4,12 @@
#include "constants.h"
#include "context.h"
+static inline double speed_of_sound(double temperature);
+static inline double calculate_retard(DragModel drag_function,
+ double ballistic_coefficient,
+ double velocity,
+ double mach);
+
double atmospheric_correction(double ballistic_coefficient,
double temperature,
double pressure,
@@ -36,3 +42,28 @@ double calculate_air_density(double temperature,
else
return pressure / (SPECIFIC_GAST_CONSTANT_DRY_AIR * temperature);
}
+
+static inline double speed_of_sound(double temperature) {
+ return sqrt(331.3 * (1.0 + temperature - 273.15 / 273.15));
+}
+
+static inline double
+calculate_retard(DragModel ballistic_model,
+ double ballistic_coefficient,
+ double velocity,
+ double mach)
+{
+ double m = velocity / mach;
+for (int i = 0
+}
+
+double retard(DragModel ballistic_model,
+ double ballistic_coefficient,
+ double velocity,
+ double temperature)
+{
+ return calculate_retard(ballistic_model,
+ ballistic_coefficient,
+ velocity,
+ speed_of_sound(temperature));
+}