PressureAltitude: PressureAltitude
In NCAR/Ranadu: Functions for use with RAF aircraft data files
PressureAltitude R Documentation
PressureAltitude
Description
Pressure altitude in the ISA standard atmosphere
Usage
PressureAltitude(P)
Arguments
P
A numeric vector representing pressure in hPa
Details
Calculates the altitude in the ISA standard atmosphere corresponding to the specified pressure
Value
A numeric vector giving the pressure altitude in meters
Author(s)
William Cooper
Examples
PALT <- PressureAltitude (500.)
PALT2 <- PressureAltitude (RAFdata$PSXC)
NCAR/Ranadu documentation built on Jan. 27, 2023, 1:09 a.m.
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| PressureAltitude | R Documentation |
PressureAltitude
Description
Pressure altitude in the ISA standard atmosphere
Usage
PressureAltitude(P)
Arguments
P |
A numeric vector representing pressure in hPa |
Details
Calculates the altitude in the ISA standard atmosphere corresponding to the specified pressure
Value
A numeric vector giving the pressure altitude in meters
Author(s)
William Cooper
Examples
PALT <- PressureAltitude (500.) PALT2 <- PressureAltitude (RAFdata$PSXC)
R Package Documentation
Browse R Packages
We want your feedback!
Note that we can't provide technical support on individual packages. You should contact the package authors for that.
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