Atmosphere.Atmosphere
— ModuleInternational Standard Atmospheric (ISA) model
Only metric units are used.
Source: EUROCONTROL BADA 4 User Manual Chapter 2.2 Atmosphere Model
Atmosphere.T₀
— ConstantStandard atmospheric temperature [K] at Mean Sea Level (MSL)
Atmosphere.a₀
— ConstantSpeed of sound [m/s] at Mean Sea Level (MSL)
Atmosphere.g₀
— ConstantGraviation acceleration [m/s²]
Atmosphere.p₀
— ConstantStandard atmospheric pressure [Pa] at Mean Sea Level (MSL)
Atmosphere.κ
— ConstantAdiabatic index of air []
Atmosphere.ρ₀
— ConstantStandard atmospheric density [kg/m³] at Mean Sea Level (MSL)
Atmosphere.Hp_trans
— FunctionHp_trans(Vcas::Float64, M::Float64, ΔT::Float64 = 0.0) Transition altitude (also called crossover altitude) [m] between a given calibrated airspeed [m/s] and a Mach number M and with temperature offset ΔT [K] EUROCONTROL BADA 4 User Manual eq. 2.2-27/28/29
Atmosphere.M2Vcas
— MethodM2Vcas(M::Float64, p::Float64, T::Float64) Calibrated airspeed Vcas [m/s] as a function of the Mach number at pressure level p [Pa] and with temperature T [K] EUROCONTROL BADA 4 User Manual eq. 2.2-26
Atmosphere.M2Vtas
— MethodM2Vtas(M::Float64, T::Float64) True airspeed Vtas [m/s] as a function of the Mach number and temperature T [K] EUROCONTROL BADA 4 User Manual eq. 2.2-26
Atmosphere.T
— FunctionT(Hp::Float64, ΔT::Float64 = 0.0) Atmospheric temperature [K] at pressure altitude Hp [m] and with temperature offset ΔT [K] EUROCONTROL BADA 4 User Manual eq. 2.2-13/16
Atmosphere.Vcas2M
— MethodVtas2M(Vtas::Float64, T::Float64) Mach as a function of the True airspeed Vtas [m/s] at pressure level p [Pa] and with temperature T [K] EUROCONTROL BADA 4 User Manual eq. 2.2-26 (reversed)
Atmosphere.Vcas2Vtas
— MethodVcas2Vtas(Vcas::Float64, p::Float64, T::Float64) True airspeed Vtas [m/s] as a function of the calibrated airspeed Vcas [m/s] at pressure level p [Pa] and with temperature T [K] EUROCONTROL BADA 4 User Manual eq. 2.2-23
Atmosphere.Vtas2M
— MethodVtas2M(Vtas::Float64, T::Float64) Mach as a function of the True airspeed Vtas [m/s] and temperature T [K] EUROCONTROL BADA 4 User Manual eq. 2.2-26 (reversed)
Atmosphere.Vtas2Vcas
— MethodVtas2Vcas(Vtas::Float64, p::Float64, T::Float64) Calibrated airspeed Vcas [m/s] as a function of the True airspeed Vtas [m/s] at pressure level p [Pa] and with temperature T [K] EUROCONTROL BADA 4 User Manual eq. 2.2-24
Atmosphere.a
— Methoda(T::Float64) Speed of sound [m/s] at pressure level [Pa] and with temperature T [K] EUROCONTROL BADA 4 User Manual eq. 2.2-22
Atmosphere.p
— Functionp(Hp::Float64, ΔT::Float64 = 0.0) Air pressure [Pa] at pressure altitude Hp [m] and with temperature offset ΔT [K] EUROCONTROL BADA 4 User Manual eq. 2.2-18/20
Atmosphere.ρ
— Methodρ(p, T) Air density [kg/m³] at pressure level [Pa] and Temperature [K] EUROCONTROL BADA 4 User Manual eq. 2.2-21
Atmosphere.Hp_trop
— ConstantGeopotential pressure altitude [m] of Tropopause
Atmosphere.R
— ConstantReal gas constant for air [M²/(Ks²)]
Atmosphere.βT∇
— ConstantISA temperature gradient [K/m] with altitude below the tropopause
Atmosphere.μ
— Constantconstant used for Vtas<->Vcas conversion
Atmosphere.δ
— Methodδ(p::Float64) pressure ratio EUROCONTROL BADA 4 User Manual eq. 2.2-31
Atmosphere.θ
— Methodθ(T::Float64) temperature ratio EUROCONTROL BADA 4 User Manual eq. 2.2-30
Atmosphere.σ
— Methodσ(ρ::Float64) density ratio EUROCONTROL BADA 4 User Manual eq. 2.2-32