Difference between revisions of "oapiGetAtmPressureDensity"
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Pressure and density are calculated using an exponential barometric equation, without accounting for local variations on [[Celestial body|celestial bodies]] without [[Atmosphere model|atmosphere model]] inside their [[Module|module]]. | Pressure and density are calculated using an exponential barometric equation, without accounting for local variations on [[Celestial body|celestial bodies]] without [[Atmosphere model|atmosphere model]] inside their [[Module|module]]. | ||
| − | [[Category:OrbiterSDK|GetAtmPressureDensity]][[Category:Aerodynamics API|GetAtmPressureDensity]] | + | [[Category: Articles]] |
| − | + | [[Category:OrbiterSDK|GetAtmPressureDensity]] | |
| + | [[Category:Aerodynamics API|GetAtmPressureDensity]] | ||
| + | [[Category:Aerodynamics]] | ||
Latest revision as of 15:49, 16 October 2022
Returns the atmospheric pressure and density at the current vessel position.
void oapiGetAtmPressureDensity (
OBJHANDLE hVessel,
double *pressure
double *density)
Parameters[edit]
- hVessel
- vessel handle
- pressure
- pointer to the variable receiving pressure value (Pa)
- density
- pointer to the variable receiving density value (kg/m^3)
Notes[edit]
Pressure and density are calculated using an exponential barometric equation, without accounting for local variations on celestial bodies without atmosphere model inside their module.