The fifth session was started with a brief explanation of C control statements by one of our friend like branching, looping and operators.
Avionics is basically a combination of all electronics and electromechanical system and subsystems installed in an aircraft or attached to it. Though the avionics system is the central integrating technology but it cannot work on all it’s on. The various requirements of the avionics can be summarized into
- Safety of the flight
- Mission of the aircraft
- Life cycle cost/cost of ownership
- Certification for flying from their respective regulatory and advisory agencies
Avionics system requirements
- Aircrafts without ejection Ex:civil aircraft probability of catastrophic failure<10^-9/flighthour
- Aircrafts with ejection Ex:civil aircraft probability of catastrophic failure<10^-7/flighthour
Military aircraft->CEMILAC
Military IFF(Identity friend or ford)-contains a special code to identify the aircraft is friend or enemy.
Next we saw the Avionic systems implemented on a multipurpose aircraft and listed out few of them as
- GPS : Global Positioning Satellite
- IFF : Identifying Friend or Foe ( it generates a specific code to differentiate between a civil or a fighter A/C
- MLS : Microwave Landing System
- Weather RADAR
- Glideslope : Part of an ILS system
- DME: Distance Measuring Equipment for giving the pilot an approx measurement of the slant distance from the runway.
- Marker beacon: Mostly installed at both the ends of the runway, provides information to the pilot about the height, distance etc during final approach in low visibility (outer marker), during missed approach (middle marker) and during arrival at the runway beginning (inner marker).
- VHF: Very High Frequency
- ATC transponder: A transmitter responder that interacts with RADAR frequency on ground giving the details about the A/C positions.
- TCAS
- Radio altimeter: Tells the height of the plane.
- Military VHF
- Line TV
- ADF: Automatic Direction Finder
- VHF satcom, C-band satcom etc.
Some of the important systems apart from the above mentioned avionic systems that were discussed include:
- Various navigation systems used, like
- Absolute navigation system
- Dead reckoning navigation system used during Visual Flight Rules.
- Mapping navigation system
- Flight control: consists of all the necessary mechanisms to control the direction of the A/C.
- Engine control
- FMS: Flight Management System stores the coordinates of en route way points and calculates the steering signals using GPS or INS to fly towards them. It can guide a plane in autopilot mode along the route and also can control the engine thrust.
- Subsystem monitoring and control
- Collision avoidance: The two important systems under these are TCAS and EGPWS.
- Weather detection using weather RADAR, lightening detection system.
- ELT: Emergency Location Transmitter gives an alarm either automatically or manually on experiencing a high-gravity impact on collision to ground or crashing. It is tuned to 121.5 (emergency frequency),243 and 406 MHz.These frequencies are monitored by search-and-rescue aircraft and by SARSAT-COSPAS satellites.
- Target sensors
- Weapon management, ECMs, mission planning and formation flight.
We then discussed about the various regulatory and advisory agencies in operation across the globe. Some of them being FAA, ICAO, FCC, RTCA, ARINC, DO-178A, DO-160D, SAE, IEEE, JAA, DGCA UK, DGAC France, DGCA India etc. After that we got an insight into anti collision system
- EGPWS (Enhanced Ground Proximity Warning System) which provides information about the surrounding terrain. We were also told about the seven modes of EGPWS i.e., excessive descent rate, excessive close to the terrain, altitude loss after take off, unsafe terrain clearance, excessive Glideslope deviation, bank angle and wind shear alerting.
7 Modes of EGPWS
- Mode 1-Excessive decent rate
- Mode 2-Excessive closure to terrain
- Mode 3-Altitude loss after take off
- Mode 4-Unsafe terrain clearance
- Mode 5-Excessive glideslope deviation
- Mode 6-Advisory callout /bank angle
- Mode 7-Wind shear alerting
- TCAS (Traffic Collision Avoidance System) which consists of traffic advisories (TAs) and resolution advisories (RAs).
Later we were shown some professional coding which derived its variables from the airbus coding standards.
The session ended with a description about the indigenous LCA-Tejas by our TL.