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Avionics-Embedded systems-basic

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very basic presentation on Avionics...

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Avionics-Embedded systems-basic

  1. 1. What Is Avionics?  Avionics are the electronic systems used on aircraft, artificial satellites, and spacecraft.  Avionic systems include communications, navigation, the display and management of multiple systems, and the hundreds of systems that are fitted to aircraft to perform individual functions.  These can be as simple as a searchlight for a police helicopter or as complicated as the tactical system for an airborne early warning platform.  The term avionics is a combination of the words aviation and electronics.
  2. 2. History of Avionics • Many modern avionics have their origins in World War II wartime developments. For example, autopilot systems that are prolific today were started to help bomber planes fly steadily enough to hit precision targets from high altitudes. • Famously, radar was developed in the UK, Germany, and the United States during the same period. • Modern avionics is a substantial portion of military aircraft spending. Aircraft like the F-15E and the now retired F-14 have roughly 20 percent of their budget spent on avionics. F-15E
  3. 3. Modern avionics • Avionics plays a heavy role in modernization initiatives like the Federal Aviation Administration's (FAA) Next Generation Air Transportation System project in the United States and the Single European Sky ATM Research(SESAR) initiative in Europe. The Joint Planning and Development Office put forth a roadmap for avionics in six areas: 1) Published Routes and Procedures – Improved navigation and routing 2) Negotiated Trajectories – Adding data communications to create preferred routes dynamically 3) Delegated Separation – Enhanced situational awareness in the air and on the ground 4) Low Visibility/Ceiling Approach/Departure – Allowing operations with weather constraints with less ground infrastructure 5) Surface Operations – To increase safety in approach and departure 6) ATM Efficiencies – Improving the ATM process
  4. 4. Aircraft avionics • The cockpit of an aircraft is a typical location for avionic equipment, including control, monitoring, communication, navigation, weather, and anti-collision systems. • The majority of aircraft power their avionics using 14- or 28-volt DC electrical systems; however, larger, more sophisticated aircraft (such as airliners or military combat aircraft) have AC systems operating at 400 Hz, 115 volts AC. • There are several major vendors of flight avionics, including Panasonic Avionics Corporation, Honeywell (which now owns Bendix/King), Rockwell Collins, Thales Group, GE Aviation Systems,Garmin, Parker Hannifin, UTC Aerospace Systems and Avidyne Corporation. • One source of international standards for avionics equipment are prepared by the Airlines Electronic Engineering Committee (AEEC) and published by ARINC.
  5. 5. Communications  Communications connect the flight deck to the ground and the flight deck to the passengers. On-board communications are provided by public-address systems and aircraft intercoms.  The VHF aviation communication system works on the airband of 118.000 MHz to 136.975MHz.Each channel is spaced from the adjacent ones by 8.33 kHz in Europe, 25 kHz elsewhere. VHF is also used for line of sight communication such as aircraft-to-aircraft and aircraft-to-ATC. Amplitude modulation (AM) is used, and the conversation is performed in simplex mode.  Aircraft communication can also take place using HF (especially for trans- oceanic flights) or satellite communication.
  6. 6. Navigation • Navigation is the determination of position and direction on or above the surface of the Earth. • Avionics can use satellite-based systems (such as GPS and WAAS), ground-based systems (such as VOR or LORAN), or any combination thereof. • Navigation systems calculate the position automatically and display it to the flight crew on moving map displays. • Older avionics required a pilot or navigator to plot the intersection of signals on a paper map to determine an aircraft's location; modern systems calculate the position automatically and display it to the flight crew on moving map displays.
  7. 7. Monitoring • The first hints of glass cockpits emerged in the 1970s when flight- worthy cathode ray tubes(CRT) screens began to replace electromechanical displays, gauges and instruments. • A "glass" cockpit refers to the use of computer monitors instead of gauges and other analog displays. • Aircraft were getting progressively more displays, dials and information dashboards that eventually competed for space and pilot attention. • In the 1970s, the average aircraft had more than 100 cockpit instruments and controls. • Glass cockpits started to come into being with the Gulfstream G-IV private jet in 1985. One of the key challenges in glass cockpits is to balance how much control is automated and how much the pilot should do manually. • Generally they try to automate flight operations while keeping the pilot constantly informed.
  8. 8. Aircraft flight-control systems • Aircraft have means of automatically controlling flight. Today automated flight control is common to reduce pilot error and workload at key times like landing or takeoff. • Autopilot was first invented by Lawrence Sperry during World War II to fly bomber planes steady enough to hit precision targets from 25,000 feet. When it was first adopted by the U.S. military, aHoneywell engineer sat in the back seat with bolt cutters to disconnect the autopilot in case of emergency. • Nowadays most commercial planes are equipped with aircraft flight control systems in order to reduce pilot error and workload at landing or takeoff. • The first simple commercial auto-pilots were used to control heading and altitude and had limited authority on things like thrust and flight control surfaces. • In helicopters, auto-stabilization was used in a similar way. The first systems were electromechanical. • The advent of fly by wire and electro-actuated flight surfaces (rather than the traditional hydraulic) has increased safety. As with displays and instruments, critical devices that were electro-mechanical had a finite life. With safety critical systems, the software is very strictly tested.
  9. 9. Collision-avoidance systems • To supplement air traffic control, most large transport aircraft and many smaller ones use a traffic alert and collision avoidance system(TCAS), which can detect the location of nearby aircraft, and provide instructions for avoiding a midair collision. • Smaller aircraft may use simpler traffic alerting systems such as TPAS, which are passive (they do not actively interrogate the transponders of other aircraft) and do not provide advisories for conflict resolution. • To help avoid controlled flight into terrain (CFIT), aircraft use systems such as ground-proximity warning systems(GPWS), which use radar altimeters as a key element. One of the major weaknesses of GPWS is the lack of "look-ahead" information, because it only provides altitude above terrain "look-down". • In order to overcome this weakness, modern aircraft use a terrain awareness warning system (TAWS).
  10. 10. Black Boxes • Commercial aircraft cockpit data recorders, commonly known as a "black box", store flight information and audio from the cockpit. • They are often recovered from a plane after a crash to determine control settings and other parameters during the incident.
  11. 11. Weather systems • Weather systems such as weather radar (typically Arinc 708 on commercial aircraft) and lightning detectors are important for aircraft flying at night or in instrument meteorological conditions, where it is not possible for pilots to see the weather ahead. • Heavy precipitation (as sensed by radar) or severe turbulence (as sensed by lightning activity) are both indications of strong convective activity and severe turbulence, and weather systems allow pilots to deviate around these areas. • Modern weather systems also include wind shear and turbulence detection and terrain and traffic warning systems. • Modern displays allow weather information to be integrated with moving maps, terrain, and traffic onto a single screen, greatly simplifying navigation.
  12. 12. Aircraft management systems • There has been a progression towards centralized control of the multiple complex systems fitted to aircraft, including engine monitoring and management. • Health and usage monitoring systems (HUMS) are integrated with aircraft management computers to give maintainers early warnings of parts that will need replacement. • The integrated modular avionics concept proposes an integrated architecture with application software portable across an assembly of common hardware modules. It has been used in fourth generation jet fighters and the latest generation of airliners.
  13. 13. Radar •Airborne radar was one of the first tactical sensors. The benefit of altitude providing range has meant a significant focus on airborne radar technologies. Radars include airborne early warning (AEW), anti-submarine warfare (ASW), and even weather radar (Arinc708) and ground tracking/proximity radar. •The military uses radar in fast jets to help pilots fly at low levels. While the civil market has had weather radar for a while, there are strict rules about using it to navigate the aircraft. Sonar •Dipping sonar fitted to a range of military helicopters allows the helicopter to protect shipping assets from submarines or surface threats. •Maritime support aircraft can drop active and passive sonar devices (sonobuoys) and these are also used to determine the location of hostile submarines.
  14. 14. Avionics software • Avionics software is embedded software with legally mandated safety and reliability concerns used in avionics. • The main difference between avionic software and conventional embedded software is that the development process is required by law and is optimized for safety.

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