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Interface: AdcEvents

Defined in: src/sdk/instruments/Adc.ts:148

Events related to air data computer information.

Extends​

Indexable​

[key: `ias_${number}`]: number

[key: `tas_${number}`]: number

[key: `indicated_tas_${number}`]: number

[key: `indicated_mach_number_${number}`]: number

[key: `mach_to_kias_factor_${number}`]: number

[key: `tas_to_ias_factor_${number}`]: number

[key: `indicated_mach_to_kias_factor_${number}`]: number

[key: `indicated_tas_to_ias_factor_${number}`]: number

[key: `indicated_alt_${number}`]: number

[key: `altimeter_baro_setting_inhg_${number}`]: number

[key: `altimeter_baro_setting_mb_${number}`]: number

[key: `altimeter_baro_preselect_inhg_${number}`]: number

[key: `altimeter_baro_preselect_mb_${number}`]: number

[key: `altimeter_baro_preselect_raw_${number}`]: number

[key: `altimeter_baro_is_std_${number}`]: boolean

Properties​

altimeter_baro_is_std​

altimeter_baro_is_std: boolean

Defined in: src/sdk/instruments/Adc.ts:61

Whether the altimeter baro setting is set to STD (true=STD, false=set pressure).

Inherited from​

BaseAdcEvents.altimeter_baro_is_std

altimeter_baro_preselect_inhg​

altimeter_baro_preselect_inhg: number

Defined in: src/sdk/instruments/Adc.ts:52

The current preselected altimeter baro setting, in inches of mercury.

Inherited from​

BaseAdcEvents.altimeter_baro_preselect_inhg

altimeter_baro_preselect_mb​

altimeter_baro_preselect_mb: number

Defined in: src/sdk/instruments/Adc.ts:55

The current preselected altimeter baro setting, in millibars.

Inherited from​

BaseAdcEvents.altimeter_baro_preselect_mb

altimeter_baro_preselect_raw​

altimeter_baro_preselect_raw: number

Defined in: src/sdk/instruments/Adc.ts:58

The current preselected altimeter baro setting, in raw units (1/16th millibar).

Inherited from​

BaseAdcEvents.altimeter_baro_preselect_raw

altimeter_baro_setting_inhg​

altimeter_baro_setting_inhg: number

Defined in: src/sdk/instruments/Adc.ts:46

The current altimeter baro setting, in inches of mercury.

Inherited from​

BaseAdcEvents.altimeter_baro_setting_inhg

altimeter_baro_setting_mb​

altimeter_baro_setting_mb: number

Defined in: src/sdk/instruments/Adc.ts:49

The current altimeter baro setting, in millibars.

Inherited from​

BaseAdcEvents.altimeter_baro_setting_mb

ambient_density​

ambient_density: number

Defined in: src/sdk/instruments/Adc.ts:64

The ambient air density, in slugs per cubic foot

Inherited from​

BaseAdcEvents.ambient_density

ambient_pressure_inhg​

ambient_pressure_inhg: number

Defined in: src/sdk/instruments/Adc.ts:70

The ambient pressure, in inches of mercury.

Inherited from​

BaseAdcEvents.ambient_pressure_inhg

ambient_temp_c​

ambient_temp_c: number

Defined in: src/sdk/instruments/Adc.ts:67

The ambient static air temperature, in degrees Celsius.

Inherited from​

BaseAdcEvents.ambient_temp_c

ambient_wind_direction​

ambient_wind_direction: number

Defined in: src/sdk/instruments/Adc.ts:82

The ambient wind direction, in degrees true.

Inherited from​

BaseAdcEvents.ambient_wind_direction

ambient_wind_velocity​

ambient_wind_velocity: number

Defined in: src/sdk/instruments/Adc.ts:79

The ambient wind velocity, in knots.

Inherited from​

BaseAdcEvents.ambient_wind_velocity

aoa​

aoa: number

Defined in: src/sdk/instruments/Adc.ts:88

The angle of attack, in degrees.

Inherited from​

BaseAdcEvents.aoa

density_alt​

density_alt: number

Defined in: src/sdk/instruments/Adc.ts:117

The density altitude, in feet

Inherited from​

BaseAdcEvents.density_alt

dynamic_pressure_inhg​

dynamic_pressure_inhg: number

Defined in: src/sdk/instruments/Adc.ts:120

The dynamic pressure, in inches of mercury

Inherited from​

BaseAdcEvents.dynamic_pressure_inhg

ias​

ias: number

Defined in: src/sdk/instruments/Adc.ts:16

The airplane's indicated airspeed, in knots.

Inherited from​

BaseAdcEvents.ias

indicated_alt​

indicated_alt: number

Defined in: src/sdk/instruments/Adc.ts:34

The airplane's indicated altitude, in feet.

Inherited from​

BaseAdcEvents.indicated_alt

indicated_mach_number​

indicated_mach_number: number

Defined in: src/sdk/instruments/Adc.ts:22

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

indicated_mach_to_kias_factor​

indicated_mach_to_kias_factor: number

Defined in: src/sdk/instruments/Adc.ts:111

The conversion factor from indicated mach to knots indicated airspeed in the airplane's current environment.

Inherited from​

BaseAdcEvents.indicated_mach_to_kias_factor

indicated_tas​

indicated_tas: number

Defined in: src/sdk/instruments/Adc.ts:28

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​

BaseAdcEvents.indicated_tas

indicated_tas_to_ias_factor​

indicated_tas_to_ias_factor: number

Defined in: src/sdk/instruments/Adc.ts:114

The conversion factor from indicated true airspeed to indicated airspeed in the airplane's current environment.

Inherited from​

BaseAdcEvents.indicated_tas_to_ias_factor

isa_temp_c​

isa_temp_c: number

Defined in: src/sdk/instruments/Adc.ts:73

The current ISA temperature, in degrees Celsius.

Inherited from​

BaseAdcEvents.isa_temp_c

mach_number​

mach_number: number

Defined in: src/sdk/instruments/Adc.ts:97

The speed of the aircraft in mach.

Inherited from​

BaseAdcEvents.mach_number

mach_to_kias_factor​

mach_to_kias_factor: number

Defined in: src/sdk/instruments/Adc.ts:103

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

on_ground​

on_ground: boolean

Defined in: src/sdk/instruments/Adc.ts:85

Whether the plane is on the ground.

Inherited from​

BaseAdcEvents.on_ground

pressure_alt​

pressure_alt: number

Defined in: src/sdk/instruments/Adc.ts:37

The airplane's pressure altitude, in feet.

Inherited from​

BaseAdcEvents.pressure_alt

radio_alt​

radio_alt: number

Defined in: src/sdk/instruments/Adc.ts:43

The airplane's radio altitude, in feet.

Inherited from​

BaseAdcEvents.radio_alt

ram_air_temp_c​

ram_air_temp_c: number

Defined in: src/sdk/instruments/Adc.ts:76

The current ram air temperature (total air temperature), in degrees Celsius.

Inherited from​

BaseAdcEvents.ram_air_temp_c

stall_aoa​

stall_aoa: number

Defined in: src/sdk/instruments/Adc.ts:91

The stall angle of attack of the current aircraft configuration, in degrees.

Inherited from​

BaseAdcEvents.stall_aoa

tas​

tas: number

Defined in: src/sdk/instruments/Adc.ts:31

The airplane's true airspeed, in knots.

Inherited from​

BaseAdcEvents.tas

tas_to_ias_factor​

tas_to_ias_factor: number

Defined in: src/sdk/instruments/Adc.ts:106

The conversion factor from true airspeed to indicated airspeed in the airplane's current environment.

Inherited from​

BaseAdcEvents.tas_to_ias_factor

vertical_speed​

vertical_speed: number

Defined in: src/sdk/instruments/Adc.ts:40

The airplane's vertical speed, in feet per minute.

Inherited from​

BaseAdcEvents.vertical_speed

zero_lift_aoa​

zero_lift_aoa: number

Defined in: src/sdk/instruments/Adc.ts:94

The zero-lift angle of attack of the current aircraft configuration, in degrees.

Inherited from​

BaseAdcEvents.zero_lift_aoa