This session was all about AVIONICS SYSTEM-AVIONICS ELECTRONICS , many advisory agencies,at the end of session we discussed about one of the avionic system-EGPWS : Enhanced Ground Proximity Warning System and also discussed in details about TCAS.
AVIONICS SYSTEM-AVIONICS ELECTRONICS
AVIONICS :definition -The cockpit of an aircraft is a major location for avionic equipment, including control,monitoring, communication, navigation, weather, and anti-collision systems. It is subsystem which includes all the software and hardware parts installed in an aircraft.
Avionics have few principle which are listed below :
1.Safety
2.Mission of Aircraft
3.Life cycle cost
4.Certification
After this we saw , different avionics system present in all aircrafts:-
AVIONICS SYSTEM-AVIONICS ELECTRONICS
Avionics is a portmanteau which literally means aviation electronics |
Avionics have few principle which are listed below :
1.Safety
2.Mission of Aircraft
3.Life cycle cost
4.Certification
After this we saw , different avionics system present in all aircrafts:-
- Navigation:
Absolute navigation system
Dead reckoning navigation system
Maping navigation system
- Flight Control
- Engine Control
- Flight Management
- Subsystem Monitoring and Control
- Collision Avoidance
- Weather Detection
Avionics system in Miltary Aircraft:
- Radar Infrared and other Target Sensors
- Weapon Management
fully integrated core avionics system |
- Electronic Cuntermeasures
- Mission Planning
- Formation Flight
Miltary Aircraft
Advisory Agencies:
The last topic of the session was EGPWS- Enhanced Ground Proximity Warning System:
seven modes of EGPWS-
TCAS is an aircraft collision avoidance system designed to reduce the incidence of mid-air collisions between aircraft. It monitors the airspace around an aircraft for other aircraft equipped with a corresponding active transponder, independent of air traffic control, and warns pilots of the presence of other transponder-equipped aircraft which may present a threat of mid-air collision (MAC). It is a type of airborne collision avoidance system mandated by the International Civil Aviation Organization to be fitted to all aircraft with a maximum take-off mass (MTOM) of over 5700 kg (12,586 lbs) or authorized to carry more than 19 passengers.
AGENCIES |
FAA Federal Aviation Administration
FCC Federal Communications Commission
RTCA Requirements and Technical Concepts in Aviation
ARINC Aeronautical Radio Incorporated
SAE Society of Automotive Engineers
IEEE Institute of Electrical and Electronics Engineers
JAA European Joint Aviation Authorities
EUROCAE European Organization of Civil Aviation Equipment
seven modes of EGPWS-
- Excessive descent rate
- Excessive closure to terrain
- Altitude loss after takeoff
- Unsafe terrain clearance
- Excessive Deviation Below Glide slope
- Advisory Callouts
- Windshear Alertin
TCAS traffic display · Vertical deviation indicator |