Adiru Vs Adc
Letโs clearly explain the difference and relationship between the ADC and ADIRU, step by step ๐
๐งญ 1๏ธโฃ The Simple Summary
| System | Full Name | What It Does | Main Data Type |
|---|---|---|---|
| ADC | Air Data Computer | Measures air pressures and temperature to calculate airspeed, altitude, Mach, etc. | Air data |
| ADIRU | Air Data Inertial Reference Unit | Combines air data (ADC part) and inertial data (gyros + accelerometers) for full navigation and attitude info | Air + motion data |
โ In short:
An ADIRU = ADC + IRS (Inertial Reference System) combined into one unit.
โ๏ธ 2๏ธโฃ What Each One Measures
| Input Sensors | ADC | ADIRU |
|---|---|---|
| Pitot pressure | โ | โ |
| Static pressure | โ | โ |
| Total air temperature (TAT) | โ | โ |
| Angle of Attack (AoA) | Sometimes | โ |
| Gyroscopes | โ | โ |
| Accelerometers | โ | โ |
| GPS (position update) | โ | โ |
๐งฎ 3๏ธโฃ What Each One Outputs
| Parameter | ADC | ADIRU |
|---|---|---|
| Indicated Airspeed (IAS) | โ | โ |
| True Airspeed (TAS) | โ | โ |
| Altitude (Pressure Alt) | โ | โ |
| Mach Number | โ | โ |
| Vertical Speed (VSI) | โ | โ |
| Attitude (Pitch, Roll) | โ | โ |
| Heading | โ | โ |
| Groundspeed | โ | โ |
| Position | โ | โ |
| Inertial acceleration | โ | โ |
โ๏ธ 4๏ธโฃ The Key Relationship
The ADIRU includes an air data function similar to an ADC โ but it also adds an inertial reference (gyros + accelerometers) that lets it:
- Know aircraft attitude (pitch, roll, yaw)
- Track movement through space (position, velocity, acceleration)
- Provide data even if pitot/static systems fail
So in modern aircraft (like Airbus A320, A350, Boeing 777, 787):
The ADC function is built into the ADIRU โ you donโt have separate ADC boxes anymore.
In older aircraft (B737 Classic, early A300s):
You had separate ADC units and IRUs (Inertial Reference Units).
๐งฉ 5๏ธโฃ Typical Modern Setup (Airbus-style)
PITOT / STATIC / TEMP / AoA
โ
โโโโโโโโโโโโดโโโโโโโโโโโ
โ ADIRU 1 โ
โ ADIRU 2 โ
โ ADIRU 3 โ
โโโโโโโโโโโโฌโโโโโโโโโโโ
โ
FMS โข PFD/ND โข Autopilot โข Stall Warning
Each ADIRU has two logical parts:
- ADR (Air Data Reference) โ airspeed, altitude, Mach
- IR (Inertial Reference) โ attitude, heading, position
Hence the name: AD + IR = ADIRU
๐ง 6๏ธโฃ Think of It Like This:
| Analogy | Function |
|---|---|
| ADC = Speedometer + Altimeter | Measures โhow fastโ and โhow highโ |
| IRU = Gyroscope + Compass + GPS | Measures โwhich way and how youโre movingโ |
| ADIRU = Both combined | One box that knows speed, altitude, attitude, heading, and position |
โ 7๏ธโฃ Quick Summary
| Feature | ADC | ADIRU |
|---|---|---|
| Measures Air Data | โ๏ธ | โ๏ธ |
| Measures Inertial Data | โ | โ๏ธ |
| Outputs Attitude / Heading | โ | โ๏ธ |
| Provides Navigation Data | โ | โ๏ธ |
| Used In Modern Jets | Older aircraft | All FBW jets |
| Example | B737 Classic | A320, A350, B777, B787 |
๐งญ Air Data Computer (ADC) โ Simple Explanation
The Air Data Computer (ADC) is like the โbrainโ that collects and processes all the air pressure and temperature data from the aircraftโs sensors.
It takes information from:
- Pitot tubes โ total (dynamic) pressure
- Static ports โ static air pressure
- Temperature probe โ outside air temperature
- Angle of Attack (AoA) sensor โ airflow angle over the wing
The ADC then calculates important air data values such as:
- Airspeed (IAS, CAS, TAS, Mach)
- Altitude (pressure altitude)
- Vertical speed
- Static air temperature (SAT)
These results are sent digitally to:
- Flight instruments (PFD, ND)
- Flight Management System (FMS)
- Autopilot and autothrust systems
- Inertial systems (INS/IRS)
This digital information allows all other systems to โspeak the same language.โ
โ๏ธ ADIRU โ Combined Modern Version
In modern airliners, the ADC and the Inertial Reference Unit (IRU) are combined into one unit called an:
๐งฉ ADIRU โ Air Data Inertial Reference Unit
This box provides both:
- Air data (speed, altitude, Mach, etc.)
- Inertial data (attitude, heading, acceleration, position)
Because the two data types work closely together โ airspeed and acceleration, for example โ itโs more efficient and accurate to have them in the same computer.
โ๏ธ ADIRS โ The Complete System
Airliners donโt rely on just one ADIRU. They usually have two or three ADIRUs for redundancy and safety, and together they form the:
ADIRS โ Air Data Inertial Reference System
This ensures:
- Backup if one unit fails
- Cross-checking for accuracy
- Continuous air and inertial data available to all flight systems
๐ง In Simple Terms
The ADC calculates air data (how fast, how high). The IRU measures movement and attitude (which way and how youโre moving). Modern aircraft combine both into an ADIRU, and several ADIRUs together form the ADIRS โ a smart, reliable system that keeps the aircraft accurately aware of its speed, altitude, attitude, and position.
โ In short:
ADC = Air Data only IRU = Inertial data only ADIRU = Both combined ADIRS = The complete network of ADIRUs for redundancy