Interface: AdcEvents
Events related to air data computer information.
Hierarchy
AdcIndexedEvents↳
AdcEvents
Properties
altimeter_baro_is_std
• altimeter_baro_is_std: boolean
Whether the altimeter baro setting is set to STD (true=STD, false=set pressure).
Inherited from
BaseAdcEvents.altimeter_baro_is_std
Defined in
src/sdk/instruments/Adc.ts:61
altimeter_baro_preselect_inhg
• altimeter_baro_preselect_inhg: number
The current preselected altimeter baro setting, in inches of mercury.
Inherited from
BaseAdcEvents.altimeter_baro_preselect_inhg
Defined in
src/sdk/instruments/Adc.ts:52
altimeter_baro_preselect_mb
• altimeter_baro_preselect_mb: number
The current preselected altimeter baro setting, in millibars.
Inherited from
BaseAdcEvents.altimeter_baro_preselect_mb
Defined in
src/sdk/instruments/Adc.ts:55
altimeter_baro_preselect_raw
• altimeter_baro_preselect_raw: number
The current preselected altimeter baro setting, in raw units (1/16th millibar).
Inherited from
BaseAdcEvents.altimeter_baro_preselect_raw
Defined in
src/sdk/instruments/Adc.ts:58
altimeter_baro_setting_inhg
• altimeter_baro_setting_inhg: number
The current altimeter baro setting, in inches of mercury.
Inherited from
BaseAdcEvents.altimeter_baro_setting_inhg
Defined in
src/sdk/instruments/Adc.ts:46
altimeter_baro_setting_mb
• altimeter_baro_setting_mb: number
The current altimeter baro setting, in millibars.
Inherited from
BaseAdcEvents.altimeter_baro_setting_mb
Defined in
src/sdk/instruments/Adc.ts:49
ambient_density
• ambient_density: number
The ambient air density, in slugs per cubic foot
Inherited from
Defined in
src/sdk/instruments/Adc.ts:64
ambient_pressure_inhg
• ambient_pressure_inhg: number
The ambient pressure, in inches of mercury.
Inherited from
BaseAdcEvents.ambient_pressure_inhg
Defined in
src/sdk/instruments/Adc.ts:70
ambient_temp_c
• ambient_temp_c: number
The ambient static air temperature, in degrees Celsius.
Inherited from
Defined in
src/sdk/instruments/Adc.ts:67
ambient_wind_direction
• ambient_wind_direction: number
The ambient wind direction, in degrees true.
Inherited from
BaseAdcEvents.ambient_wind_direction
Defined in
src/sdk/instruments/Adc.ts:82
ambient_wind_velocity
• ambient_wind_velocity: number
The ambient wind velocity, in knots.
Inherited from
BaseAdcEvents.ambient_wind_velocity
Defined in
src/sdk/instruments/Adc.ts:79
aoa
• aoa: number
The angle of attack, in degrees.
Inherited from
Defined in
src/sdk/instruments/Adc.ts:88
density_alt
• density_alt: number
The density altitude, in feet
Inherited from
Defined in
src/sdk/instruments/Adc.ts:117
ias
• ias: number
The airplane's indicated airspeed, in knots.
Inherited from
Defined in
src/sdk/instruments/Adc.ts:16
indicated_alt
• indicated_alt: number
The airplane's indicated altitude, in feet.
Inherited from
Defined in
src/sdk/instruments/Adc.ts:34
indicated_mach_number
• indicated_mach_number: number
The airplane's mach number, as calculated from the impact pressure derived from the current indicated airspeed and ambient pressure.
Inherited from
BaseAdcEvents.indicated_mach_number
Defined in
src/sdk/instruments/Adc.ts:22
indicated_mach_to_kias_factor
• indicated_mach_to_kias_factor: number
The conversion factor from indicated mach to knots indicated airspeed in the airplane's current environment.
Inherited from
BaseAdcEvents.indicated_mach_to_kias_factor
Defined in
src/sdk/instruments/Adc.ts:111
indicated_tas
• indicated_tas: number
The airplane's true airspeed, in knots, as calculated from the impact pressure derived from the current indicated airspeed, ambient pressure, and ambient temperature.
Inherited from
Defined in
src/sdk/instruments/Adc.ts:28
indicated_tas_to_ias_factor
• indicated_tas_to_ias_factor: number
The conversion factor from indicated true airspeed to indicated airspeed in the airplane's current environment.
Inherited from
BaseAdcEvents.indicated_tas_to_ias_factor
Defined in
src/sdk/instruments/Adc.ts:114
isa_temp_c
• isa_temp_c: number
The current ISA temperature, in degrees Celsius.
Inherited from
Defined in
src/sdk/instruments/Adc.ts:73
mach_number
• mach_number: number
The speed of the aircraft in mach.
Inherited from
Defined in
src/sdk/instruments/Adc.ts:97
mach_to_kias_factor
• mach_to_kias_factor: number
The conversion factor from mach to knots indicated airspeed in the airplane's current environment. In other words, the speed of sound in knots indicated airspeed.
Inherited from
BaseAdcEvents.mach_to_kias_factor
Defined in
src/sdk/instruments/Adc.ts:103
on_ground
• on_ground: boolean
Whether the plane is on the ground.
Inherited from
Defined in
src/sdk/instruments/Adc.ts:85
pressure_alt
• pressure_alt: number
The airplane's pressure altitude, in feet.
Inherited from
Defined in
src/sdk/instruments/Adc.ts:37
radio_alt
• radio_alt: number
The airplane's radio altitude, in feet.
Inherited from
Defined in
src/sdk/instruments/Adc.ts:43
ram_air_temp_c
• ram_air_temp_c: number
The current ram air temperature (total air temperature), in degrees Celsius.
Inherited from
Defined in
src/sdk/instruments/Adc.ts:76
stall_aoa
• stall_aoa: number
The stall angle of attack of the current aircraft configuration, in degrees.
Inherited from
Defined in
src/sdk/instruments/Adc.ts:91
tas
• tas: number
The airplane's true airspeed, in knots.
Inherited from
Defined in
src/sdk/instruments/Adc.ts:31
tas_to_ias_factor
• tas_to_ias_factor: number
The conversion factor from true airspeed to indicated airspeed in the airplane's current environment.
Inherited from
BaseAdcEvents.tas_to_ias_factor
Defined in
src/sdk/instruments/Adc.ts:106
vertical_speed
• vertical_speed: number
The airplane's vertical speed, in feet per minute.
Inherited from
Defined in
src/sdk/instruments/Adc.ts:40
zero_lift_aoa
• zero_lift_aoa: number
The zero-lift angle of attack of the current aircraft configuration, in degrees.
Inherited from
Defined in
src/sdk/instruments/Adc.ts:94