fix MEAS airspeed and airspeed calibration

This commit is contained in:
Thomas Gubler
2013-11-10 19:24:37 +01:00
parent c63995e91c
commit ae9fae5aae
7 changed files with 52 additions and 13 deletions
+1 -1
View File
@@ -59,7 +59,7 @@
float calc_indicated_airspeed(float differential_pressure)
{
if (differential_pressure > 0) {
if (differential_pressure > 0.0f) {
return sqrtf((2.0f*differential_pressure) / CONSTANTS_AIR_DENSITY_SEA_LEVEL_15C);
} else {
return -sqrtf((2.0f*fabsf(differential_pressure)) / CONSTANTS_AIR_DENSITY_SEA_LEVEL_15C);