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ELEC4504/4906G AVIONICS SYSTEMS ENGINEERING

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Title: ELEC4504/4906G AVIONICS SYSTEMS ENGINEERING


1
ELEC4504/4906GAVIONICS SYSTEMS ENGINEERING
2
INTRODUCTION
  • OBJECTIVES
  • SOME HISTORY
  • FACTORS AFFECTING AVIONICS DEVELOPMENT

3
COURSE OBJECTIVES
  • To provide the aeronautical engineering student
    with knowledge of
  • The basic principles behind the avionics systems
    used in civil aircraft
  • The factors which should be taken into account
    when installing avionics in aircraft and
  • How the avionics systems are used in the
    operation of a commercial aircraft

4
COURSE OUTLINE
  • Organizational Framework
  • Air Traffic Control
  • CNS Communications/ Navigation /Surveillance
  • The Electromagnetic Spectrum
  • Navigation
  • Precision Approach Systems
  • Communications Systems
  • Radar and Surveillance Systems

5
COURSE OUTLINE(CONTINUED)
  1. Control Systems
  2. Flight Management Systems
  3. Display Systems
  4. Electrical Systems
  5. System Design
  6. System Testing
  7. Future Developments

6
Factors Affecting Avionics Development
Sometimes it appears to take a long time to
introduce new systems into service. There are
several reasons for this
  1. Cost
  2. Number of systems in service
  3. Benefits
  4. Reliability

7
ORGANIZATIONAL FRAMEWORK
  1. ICAO (International Civil Aviation Organization)
  2. National Civil Aviation Organizations (FAA, CAA,
    Transport Canada).
  3. RTCA
  4. SAE
  5. ARINC
  6. EUROCAE

8
ORGANIZATIONAL FRAMEWORK
  • ICAO (International Civil Aviation Organization)
  • Part of the United Nations
  • Headquarters in Montreal
  • Since civil aviation is an international
    activity, it is beneficial for all nations to use
    the same standards for most aspects of their
    aviation operations.

9
ICAO
  • ICAO provides this service through documents
    called SARPS (standards and recommended
    practices)
  • Examples of activities covered by SARPS are
  • Aircrew licensing
  • Weather reports
  • Flight plan forms
  • Registration Markings
  • Navigation Systems

10
ICAO
  • ICAO (Continued)
  • For example the SARPs on Navigation defines the
    characteristics of the Instrument Landing System
    (ILS) and includes
  • Signal strength
  • Signal format
  • Accuracy
  • Coverage (distances at which usable signal can be
    detected)

11
ICAO
  • ICAO (Continued)
  • Note that all of these documents are
    recommendations only. Each country (or state)
    makes its own laws and rules
  • It is advantageous, however, for a country to
    follow these SARPS since non-standard practices
    discourage other countries from operating into
    such states.

12
ORGANIZATIONAL FRAMEWORK
  • 2. RTCA (Requirements and Technical Concepts for
    Aviation)
  • Formerly known as the Radio Technical Committee
    for Aeronautics
  • and Radio Technical Commission for Aeronautics
  • An example of the FAAs practice of contracting
    out much of its technical work
  • To understand the role of RTCA it is necessary to
    understand the FAAs TSO (Technical Standard
    Order)

13
RTCA
  • A given TSO is a minimum performance standard for
    a given piece of aircraft equipment (not
    restricted to avionics equipment)
  • A TSO authorization is the FAAs recognition that
    a given design meets the TSO and also authorizes
    the manufacturer to produce it.
  • While the TSO authorization is not an approval to
    install the equipment it gives the equipment a
    very great advantage in obtaining certification
    for its installation
  • One of the first questions you are asked, if you
    want to install some equipment in an aircraft is
    is it TSOd?
  • Thus a TSO is very important

14
RTCA
  • Q Where do TSOs come from?
  • A RTCA
  • When the FAA determines the need for a new piece
    of equipment e.g. a GPS receiver, it contacts the
    RTCA.
  • RTCA then establishes a committee (called a
    special committee) and invites anyone with any
    interest in the subject to join the committee.
    (airlines, equipment manufacturers, FAA
    officials, aircraft associations and
    international representatives)
  • GPS committee is SC-159
  • The committee produces a document called a MOPS
    (minimum operational performance standard) This
    is given a number preceded by DO
  • e.g. the MOPS for the GPS receiver is DO-208

15
RTCA
  • The RTCA MOPS is then submitted to the FAA which
    uses it as the basis for the TSO
  • The GPS receiver TSO is TSO-C129a
  • Thus the RTCA is a very powerful organization in
    the development of aircraft equipment (not just
    avionics)

16
ORGANIZATIONAL FRAMEWORK
  • ARINC (Aeronautical Radio Inc)
  • Started in the 1930s by a group of airlines to
    provide communications between their aircraft and
    their bases.
  • It still provides this service through the ATN
    (Aeronautical Telecommunications Network) and
    ACARS (Aircraft Communications and Addressing
    System)
  • For avionics, however it is important for
    standardizing aircraft electronics boxes, trays
    and connectors.
  • Later it developed standards for aircraft digital
    data busses.

17
ARINC
  • ARINC (Aeronautical Radio Inc)
  • Started in the 1930s by a group of airlines to
    provide communications between their aircraft and
    their bases.
  • It still provides this service through the ATN
    (Aeronautical Telecommunications Network) and
    ACARS (Aircraft Communications and Addressing
    System)
  • For avionics, however it is important for
    standardizing aircraft electronics boxes, trays
    and connectors.

18
ARINC
  • ARINC (Aeronautical Radio Inc)
  • Started in the 1930s by a group of airlines to
    provide communications between their aircraft and
    their bases.
  • It still provides this service through the ATN
    (Aeronautical Telecommunications Network) and
    ACARS (Aircraft Communications and Addressing
    System)
  • For avionics, however it is important for
    standardizing aircraft electronics boxes, trays
    and connectors.

19
ARINC
  • Electronic Equipment in aircraft has to be
  • Firmly attached to the aircraft structure (by
    means of racks)
  • Wired in to the aircraft systems
  • Power
  • Signals
  • Controls

20
ARINC
  • Early Electronic Equipment was not standardized
    and hence the mounting systems and connectors
    were different not only for each piece of
    equipment but for the same equipment from
    different manufacturers
  • Thus upgrading equipment was expensive and time
    consuming
  • ARINC devised a set of standard black box sizes
    and corresponding mounting systems as well as
    connector designs.

21
ARINC
  • With standardized racks, boxes, trays and
    connectors, airlines could choose among various
    manufacturers of a particular item (e.g.
    Communications Transceiver) knowing that all they
    had to do was pull out the old set and plug in
    the new one.

22
ARINC
  • The original standard was called ARINC 404.
  • Or ATR (Air Transport Racking)
  • Black box sizes were 1ATR, 3/4ATR, ½ ATR, ¼ ATR
    etc.
  • A 1ATR box was about 10 wide, 8high and 22
    deep
  • The latest racking standard is ARINC 600 series.

23
ARINC
  • With the advent of digital communications in
    aircraft, ARINC developed popular digital data
    bus communications standards, primarily ARINC 429
    and ARINC 629

24
SAE
  • SAE (originally Society of Automotive Engineers,
    now SAE International)
  • Another organization which develops standards.
  • For avionics the primary publications are ARPs
    (Aerospace Recommended Practices)
  • ARP5672 - Aircraft Precipitation Static
    Certification
  • AS 5672A - ARC Fault Circuit Breaker (AFCB),
    Aircraft, Trip-Free Single Phase and Three Phase
    115 VAC, 400 Hz - Constant Frequency

25
EUROCAE
  • EUROCAE is essentially the European version of
    RTCA
  • The two organizations work closely together and
    publish joint standards.

26
AIR TRAFFIC CONTROL (ATC)AND ITS RELATIONSHIP TO
AVIONICS SYSTEMS
27

OBJECTIVES OF ATC
  • Maintain separation of aircraft
  • Expedite the flow of Air Traffic
  • NOT responsible for the separation of aircraft
    from the ground (except when in radar contact

28

RESPONSIBILITES OF THE PILOT (GENERAL)
  • Maintain aircraft ATTITUDE
  • Navigate the aircraft from departure to
    destination
  • Avoid collision with other aircraft
  • How these are accomplished depends on the weather
  • (specifically ceiling and visibility)

29
VISUAL METEOROLOGICAL CONDITIONS (VMC)
  • Generally 3 miles visibility and 1000 Ft. ceiling
  • Visual Flight Rules (VFR) apply
  • Attitude maintained by visual reference to the
    horizon
  • Navigation by reference to the ground (or
    electronic aids if pilot is able to and aircraft
    is so equipped
  • Separation from other aircraft by visual contact
    (see and be seen) Note ATC will assist but is
    not responsible.
  • Aircraft not allowed to enter cloud

30
VFR ON TOP
  • With extra training in radionavigation, pilots
    can fly in clear air above cloud
  • Note Attitude is still with reference to the
    visible horizon
  • Climb and descent must not require entry into
    cloud

31
INSTRUMENT METEOROLOGICAL CONDITIONS (IMC)
  • IMC exist whenever VMC do not
  • Obviously the rules pertaining to IMC are IFR
    (Instrument Flight Rules)
  • IFR apply in IMC and also to all flight above
    18000 Ft in Canada and the USA (other altitudes
    are specified in other countries)

32
INSTRUMENT FLIGHT RULES
  • Separation from other aircraft is responsibility
    of ATC
  • ATC issues clearances which are specific
    routes/altitudes which must be followed.
  • Attitude (pitch, bank and heading) is maintained
    with reference to instruments.
  • Simplest artificial horizon and compass
  • More complex inertial navigation system
  • Navigation is done using electronic navigation
    aids
  • Two way communication is required between pilot
    and controller
  • ATC must know where aircraft is
  • ATC radar requires a transponder on the aircraft

33
INSTRUMENT FLIGHT RULES
  • On-board Collision Avoidance Systems supplement
    ATC
  • Terrain Avoidance Systems provide protection from
    CFIT (Controlled Flight Into Terrain) when
    aircraft is out of radar coverage

34
Typical IFR Flight Procedure
  • Pilot plans route (including altitudes) from
    departure point to destination
  • Pilot files flight plan
  • ATC decides if flight plan can be accepted as is
    or if it needs to be amended
  • Prior to starting engines, pilot requests ATC
    clearance.
  • ATC gives clearance (may be just flight planned
    route)
  • Pilot contacts ground control for taxi clearance

35
Typical IFR Flight Procedure
  • Aircraft taxis to runway
  • Takeoff clearance is obtained from Tower
  • After takeoff, pilot contacts Departure Control
    who gives vectors or a series of headings and
    altitudes to guide aircraft to the start of the
    route to which it has been cleared
  • Near destination, Arrival Control provides
    vectors to the landing approach.
  • Tower gives clearance to land
  • Ground Control gives clearance to taxi to arrival
    gate
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