Avionics Flight managment system

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Flight Management System (FMS) OSTROUMOV IVAN - AVIONICS 1 www.OSTROUMOV.co.cc OSTROUMOV IVAN

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Transcript of Avionics Flight managment system

Page 1: Avionics Flight managment system

Flight Management System (FMS)

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TACAN

NDB VOR DME

GNSS WAAS LAAS EGNOS GPS GLONASS

Radio navigation Inertial navigation Satellite navigation Integrated navigation Instrument landing system

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Typical Flight Management System

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FMS control and display interface

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ТУ - 214

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Boeing 777 OSTROUMOV IVAN - AVIONICS 6

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FMS FUNCTIONS

Navigation Performance Guidance

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Navigation

• Navigation data base is in the FMC memory (Aiways, Airports, Runway, Procedures, Winds,

Flight plans) • FMC calculates the airplane position during

the flight (GPS, GLONAS, WAAS, VOR/DME, INS, NDB)

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Performance • The flight crew puts this data in the FMC:

– Airplane gross weight – Cruise altitude – Cost index.

• FMC uses the data to calculate these functions: – Economy speeds – Best flight altitude – Top of descent point.

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Guidance

• FMC sends commands to the digital flight control system and the autothrottle

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Summary of FMS capabilities

• Lateral navigation (LNAV) • Vertical navigation (VNAV) • Four-dimensional navigation • Full performance-based navigation • Future Air Navigation System (FANS)

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Lateral navigation (LNAV)

– The ability to navigate laterally in two dimensions

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Vertical navigation (VNAV)

– The ability to navigate laterally in two dimensions, plus the ability to navigate in the vertical plane. When combined with LNAV this provides three-dimensional navigation

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Four-dimensional navigation – The ability to navigate in three dimensions, plus

the addition of time constraints for the satisfaction of time of arrival at a waypoint

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Full performance-based navigation – The capability of four-dimensional navigation

together with the addition of an aircraft-specific performance model. By using cost indexing techniques, full account may be taken of the aircraft performance in real time during flight, allowing optimum use of fuel and aircraft energy to achieve the necessary flight path

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Future Air Navigation System (FANS)

– The combination of the full performance model together with all the advantages that FANS will confer, eventually enabling the concept of “free flight”

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FMS modes

THALES

Examples of FMS mode are: •Standard Instrument Departure (SID). •En route procedures. •Standard Terminal Approach Routes (STARs). •ILS approach.

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Rocwell colins

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AMS-5000 • is Designed for the intermediate-range

business aircraft. • ease of operation in today's complex

and demanding operating environment • full flight phase, multiple waypoint

vertical navigation; databased departure procedures, standard terminal arrival routes and approaches; and integrated electronic flight instrument system and radar control.

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FMS-3000 • is designed specifically for the

short-range business aircraft • full flight phase, multiple

waypoint vertical navigation; time/fuel planning and predictions based on the airplane's flight manual data; databased departure procedures, standard terminal arrival routes and approaches; and integrated electronic flight instrument system and radar control

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FMS-4200 • is designed specifically to

meet the needs of the demanding regional airline environment

• Flight planning and navigation information is presented on multifunctional display pages in front of the flight crew, allowing them to remain eyes-up during all phases of flight.

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FMS-5000

• With GPS receiver • Optimized to deliver the

navigation and performance information pilots need, as it's needed, the FMS-5000 reduces pilot workload, provides enhanced situational awareness and exceptional fly-anywhere navigational accuracy.

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FMS-6000

• is designed specifically for the business aircraft flight deck

• It is, quite simply, one of the most powerful flight planning, performance management and navigation tools available on today’s business aircraft flight deck.

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THALES

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• installed on Airbus (A318/319/320/321), provides

• Flight Management (FM) and Flight Guidance (FG) functions.

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• The main FM functions are: – Navigation, – Flight planning, – Performance prediction and optimization, – Provision of information to cockpit displays (MCDU, ND, PFD) – Auto-tuning of navaids.

• The main FG functions are: – Flight Director (FD), – Auto Pilot (A/P), – Auto thrust (A/THR) commands.

In addition, the total system provides fault isolation and detection.

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Universal Avionics Systems

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WAAS/SBAS-FMS

• WAAS/SBAS-FMSs combine the benefits of advanced programming; compact, lightweight packaging and installation flexibility. UAS produces three basic models provide you with the ability to select the optimum system to meet your desired features and capabilities and match your aircraft equipment interface requirements.

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• all-in-one-package and the navigation computer with in GPS/ WAAS receiver all in a single unit.

• The system includes a graphics- and video-capable 5-inch diagonal display with a housing depth approximately 9 inches.

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• Consists of a Fiat Panel Control Display Unit (FPCDU) and a remotely mounted navigation computer unit.

• Three FPCDUs are available: a compact FPCDU – with 4-inch color display, – standard FPCDU with 5-inch color

display – Multi-Function CDU (MCDU).

• All CDUs provide graphics support for weather images as well as video display capabilities for TAWS and camera interfaces. The 4- and 5-inch FPCDUs are both just 3 1/4 inches deep.

• The navigation computer is housed in a 2-MCU sized Line Replaceable Unit (LRU) which includes the Integral GPS/ WAAS receiver.

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• Is comprised of a 4- or 5-inch FPCDU and remotely mounted navigation computer.

• The navigation computer is housed in a 2-MCU sized line Replaceable Unit (LRU) which includes the integral GPS/WAAS receiver.

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Honeywell

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GNS-XLS FMS

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GNS-XLS FMS

• integrated system designed to give the pilot centralized control for – the navigation sensors, – computer based flight planning, – fuel management, – radio management.

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GNS-XLS FMS • full color flat panel LCD display, • alpha-numeric and function keys, • Global Positioning Sensor (GPS), • navigation data base.

All these are housed in a panel/pedestal

mounted Control Display Unit (CDU).

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№ Departure Arrived Date /time

Kiev, Borispol Эркан, Кипр, Lefkosa 1 September 2009/ 8:10

Donetsk Дару, Папуа - Новая Гвинея, Дару 10 September 2010/ 9:20

Lvov Blonduos, Исландия, Blonduos 2 October 2008/ 10:05

Odessa Брэндон, Канада, Брэндон 12 October 2007/ 11:15

Zaporozhye, Mokraya Oshawa, Канада, Oshawa 3 November 2009/ 12:07

Vinnitsa Аэропорт Брюсселя, Бельгия,

Брюссель 4 November 2010/ 13:09

Cherkasy ScotRail, Великобритания, Glasgow 5 December 2009/ 12:17

Dnipropetrovsk Херингсдорф, Германия, Херингсдорф 7 December 2010/ 14:05

Ivano-Frankivsk Zoersel, Бельгия, Zoersel 20 January 2009/ 15:24

Kharkiv, Osnova Bounneua, Лаос, Phongsaly 23 January 2010/ 16:21

Kiev, Zhulyany Kortrijk, Бельгия, Kortrijk 7 February 2009/ 17:23

Kryvyi Rih Lozovatka Shekou Port, Китай, Shekou 25 February 2010/ 18:29

Mykolaiv Ронда, Испания, Ронда 12 March 2009/ 19:17

Simferopol Кусамо, Финляндия, Кусамо 15 April 2010/ 20:19

Rovno Montilla, Панама, Montilla 25 May 2009/ 22:21

Uzhgorod Бонте, Сьерра-Леоне, Бонте 11 June 2010/ 23:29