PressureAltitude: PressureAltitude
In WilliamCooper/Ranadu: Functions for use with RAF aircraft data files
Description
Usage
Arguments
Details
Value
Author(s)
Examples
Description
Pressure altitude in the ISA standard atmosphere
Usage
1
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
1
2
PALT <- PressureAltitude (500.)
PALT2 <- PressureAltitude (RAFdata$PSXC)
WilliamCooper/Ranadu documentation built on July 10, 2019, 12:40 a.m.
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Description Usage Arguments Details Value Author(s) Examples
Description
Pressure altitude in the ISA standard atmosphere
Usage
1 |
Arguments
P |
A numeric vector representing pressure in hPa |
Details
Calculates the altitude in the ISA standard atmosphere corresponding to the specified pressure
Value
A numeric vector giving the pressure altitude in meters
Author(s)
William Cooper
Examples
1 2 | PALT <- PressureAltitude (500.)
PALT2 <- PressureAltitude (RAFdata$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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