ATM International & Airports ADSB, WAM, MLAT ...Indra’sMODES TRANSPONDER Systems CONTROLER...

ADSB, WAM, MLAT

ATM International & Airports

ADSB, WAM, MLAT implementations. ADSB/WAM integrationwith Indra’s ATC Systems

Taller OACI/FAA sobre Implementación ADS-B y Multilateración (Ciudad de México, México, 6 al 8 sept.

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INDEX

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01 ADS-B – Ground Station System

02 MLAT – Multilateration System

03 WAM – Wide Area Multilateration System

04 System Diagnosis and Tools

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05 ADS-B/MLAT/WAM Systems in Operation

06 AIRCON integration with ADS-B MLAT Systems

07 Indra’s View on MSSR/ADS/MLAT evolution

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FUNCTIONAL PROTOTYPE OF

SSR MODE S IN ELEMENTARY

SURVEILLANCE (ELS)Mode S Transponder

Selective Interrogation

Flight Plan Identification

MSSR MODE S WITH

IMPROVED SURVEILLANCE

(EHS)MAGNETIC Heading

Selected Altitude

Track Angle Rate

Ground Speed

Air Speed

Vertical Rate

Roll Angle

Indra Surveillance Products

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Flight Plan Identification

100 MODE S TRANSPONDERS

INSTALLED

“Full Mode S capability”

Peak Power: 34 dBW.

Working Cycle in 2,4 ms: 66%

Continuous Work Cycle: 6,6%.

MTBF > 20.000 hr

MSSR IRS-20MPLVA 20 dB

MSSR IRS-20MP/LLVA 27 dB (3rd. Gen)

Three Racks

Centralized Supervision and

Control

UTC Sync. by GPS

MODE S TRANSPONDER FOR

THE POEMS PROGRAM

Roll Angle

True Track Angle

ASR12ARS12 Improved

WAMVigilant(Roke)

MLAT

Barcelona,

39 Receptor Stations

6 Transmiting Est.

6 Transponders

Data Link with SMR

MSSR IRS-20MP/LLVA 24 dB (2nd. Generation)

Two racks

Open Architecture

Half angle monopulse detection

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SMRContinuous Wave

Output Power: 5 W

Resolution: 6 m

1980 1990 2000 2010

SSR IRS-10Conventional SSR

Long service Life

(1978-2004)

LVA 20 dB

Phase Monopulse Detec.

TMA

THE POEMS PROGRAM

(EUROCONTROL)

ADS-B Coverage 250 NM

Over 500 Targets

Data Link with SMR

FUNCTIONAL PROTOTYPE OF

Indra’s MODE S

TRANSPONDER

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CONTROLER INFORMATION DISPLAY

01 ADS-B – Ground Station System Product Overview

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� En-Route, TMA, approach and surface

ADSB-GSS: AUTOMATIC DEPENDANT SURVEILLANCE BROADCAST GROUND STATION SYSTEM


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� En-Route, TMA, approach and surface

surveillance applications.

� High density traffic supported, process

more than 500 targets per second.

� Use of three directional antennas

like one omni-directional antenna:

helps to reduce interferences.

�

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� Operation as Stand-alone or co-mounted with a Secondary

RADAR.

� Full solid-state technology and COTS based.

� Short term delivery and commissioning.

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Complete ADSB-GSS Site, Communications and C&M System

ADSB-GSS: AUTOMATIC DEPENDANT SURVEILLANCE BROADCAST GROUND STATION SYSTEM

ADS-B STATION ATCC


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PERSONALPERSONALPERSONALPERSONAL

COMPUTERCOMPUTERCOMPUTERCOMPUTER

GPS

ANTENNA

ADS-B SENSOR

RADAR MAINTENANCE

DISPLAY

REMOTE CONTROL AND

MONITORING POSITIONS

SRG SRG

REMOTE RADAR REMOTE RADAR REMOTE RADAR REMOTE RADAR

COMMUNICATIONSCOMMUNICATIONSCOMMUNICATIONSCOMMUNICATIONS

SYSTEM (x2)SYSTEM (x2)SYSTEM (x2)SYSTEM (x2)

GPS

ANTENNA

ADS-B SECTORIZED

ANTENNA

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LOCAL RADAR LOCAL RADAR LOCAL RADAR LOCAL RADAR

COMMUNICATIONSCOMMUNICATIONSCOMMUNICATIONSCOMMUNICATIONS

SYSTEM (x2)SYSTEM (x2)SYSTEM (x2)SYSTEM (x2)

PRINTERPRINTERPRINTERPRINTER

DIESEL

GENERATOR

AUXILIARY EQUIPMENTAUXILIARY EQUIPMENTAUXILIARY EQUIPMENTAUXILIARY EQUIPMENT

AIR

CONDITIONINGUPS

INTRUDER

ALARM

IAUIAUIAUIAU

WAN(Ethernet,

HDLC, X.25, Frame

Relay)

LOCAL CONTROL AND


SLG SLG

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� Two identical channels for redundancy and high MTBF.

Main Characteristics


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� Two identical channels for redundancy and high MTBF.

� High degree of integration (URPA):

� Small Receiver Card called TRPG with PCI interface and three independent channels.

� Digital Video Processing based on very high density FPGA.

� COTS x86 PC Processor Standard.

� GPS Card COTS integrated in the core unit called URPA with NTP Service.

� Easy Maintenance:

� Low number of LRUs (8 units).

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� Low number of LRUs (8 units).

� Simple Modular Design.

� ICAO DF 1090ES data input and ASTERIX cats. 021, 023 and 247 format and standard protocol for data output.

Sys

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sCoverage > 200 NM range

Up to 250 instrumental range

Features


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Up to 250 instrumental range

Antennas Configurable, 1 to 9 antennas

Omni-directional or directive

Target Capacity ≥ 500 aircraft

Latency < 250 ms

Update rate Configurable, minimum 0.5s.

Status Monitoring SNMP, ASTERIX 023, ASTERIX 247

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Status Monitoring SNMP, ASTERIX 023, ASTERIX 247

Data Output Format ASTERIX 021 (all versions)

Data Link 1090 Extended Squitter

Time reference UTC coupled with subsystem GPS antenna

Sys

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sReceiver Frequency: 1090MHz ± 5MHz

Sensitivity: Better than 87dBm (typical -90dBm)

Features


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Sensitivity: Better than 87dBm (typical -90dBm)

RX Channels: >3

Noise Figure <3dB

Dynamic range: 71dB

Interoperability Mode-S Radar, A-SMGCS, TIS-B and FIS-B.

High Technology Fault resistant

PC based architecture

COTS based equipment

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Communications Two redundant LAN

Based on SDCS from Indra

Redundancy Different redundant configuration.

Sys

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sAvailability: >.999997

Workload and Availability


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Integrity:>.99999

MTBCF: (reliability) > 167.598h

MTTR: (maintainability) < 15 Minutes

n x RF ports for connection to the 1090MHz

antennas.

1 x RF port for connection to the GPS antennas.

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INTERFACES:

1 x RF port for connection to the GPS antennas.

2 x RJ45 – LAN connection – ASTERIX UDP.

2 x RS232.

Panel status information with leds.

Graphical interface with management system

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MAIN INTERFACES

ICAO DF17, DF18 & DF19


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ASTERIX Cat. 021

ATCC

ADS-B

SERVICE

MANAGEMENT

SERVICE

ICAO DF17, DF18 & DF19

ASTERIX Cat. 023

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SERVICEASTERIX Cat. 247

SNMPAGENT SLAVE

Sys

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s� Minimal configuration:

�


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� 1 x antenna unit:

� Omnidirectional antenna.

� Up to 160 NM with less gain.

� 1 x process unit:

� Prepared to mount up to three sectorized channels

(standard configuration) without additional processing

hardware.

� GPS board include.

Antenna

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� GPS board include.

�Management embebed.

� Lowest cost.

Process unit

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Antenna


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� First upgrade level:

� Add up to three directional antenna: Increase the

performance in the coverage.

� Add local CMS.

Process unitLocal CMS

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Antenna

� Second upgrade level:

� Add redundancy: Install another process

unit runs in backup and a radiofrequency

switch to commutation.


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switch to commutation.

Switch

Local CMS

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Process unit 2

14

Process unit 1

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� Third upgrade level:

Antenna

Antenna


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� Double redundancy:

Install two independent

reception channels

with two antennas.

Local CMS

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with two antennas.

� Complete equipment:

- UPSs

- SDCSs

Auxiliary subsystems

Sys

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s� Vertical scalability:

�


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� Process channels: Up to six parallel channels to reduce the

high level fruit effects.

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Standard configuration Upgraded configuration

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� 2 x complete antenna

with several directional

antenna columns.

� 2 x system channels

mounted as high

availability process

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availability process

cluster.

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� Horizontal scalability:

� ADS-B Server: System developed to fusion data from ADS-B

sensors. Supplies a permanent interface with ATC to increase

scalability of the Global System.


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scalability of the Global System.

ATC

ADS-B

Server

Persistant interface

Sensor 1

Sensor 2

Sensor n

ASTERIX

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ATCASTERIX

Sensor n

Sensor n+1

Sensor n+2

Add

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ADVANTAGES OF ADS-B

� Less cost of equipment: Based on inexpensive

system components with PC architecture.


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system components with PC architecture.

� Less infrastructure cost: A single reception

station is enough to cover the equivalent Mode S

MSSR range (250NM).

� Less maintenance cost: No moving parts

involved.

� Refresh rate: Less that one second as opposed

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�to 4 seconds for MSSR.

� Optimal usage of radio spectrum: no

information is sent out to interrogate aircrafts.

� It allows to control Air Traffic in areas where

MSSR is not available and it is not viable to install

MSSR.

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� Dependant on GPS service

� Availability of Equipment: Even though the number of aircratfs


DRAWBACKS OF ADS-B

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� Availability of Equipment: Even though the number of aircratfs

equiped with ADS-B is growing, there is still a significant amount of

aircrafts not equipped with ADS-B.

� Maturity of Technology:

� There is still a large

number of aircrafts that

present errors on the

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present errors on the

information sent.

� ADS-B standards are still

under revision.

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INDEX

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Sys

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s�INDEPENDENT: Aircraft position is

calculated from the ground , and is

02 MLATSystem - Product Overview

MLAT TECHNOLOGY IS INDEPENDENT AND COOPERATIVE

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calculated from the ground , and is

therefore independent of the avionics.

�COOPERATIVE: It requires a

transponder onboard the aircraft.

•At least FOUR antennas are requires to

calculate a 3D aircraft position.

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calculate a 3D aircraft position.

•Where aircraft altitude is know, like in

airports, THREE antennas are enough for

position calculation.

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� Surface and approach surveillance

MLAT SYSTEMMULTILATERATION SYSTEM – LOCAL AREA


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� Surface and approach surveillance

applications

� High density surface traffic

supported

� Elementary and Enhanced Mode

S Surveillance functionality

� Operation as Stand-alone as part

of A-SMGCS Image from www.multilateration.org

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of A-SMGCS

� Full solid-state technology

� Short term delivery and

commissioning

Image from www.multilateration.org

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Complete Site Equipment, Communications and C&M System

MLAT SYSTEMMULTILATERATION SYSTEM – LOCAL AREA


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Sys

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s� High positional accuracy.

�



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� Local TOA measurement based on Oven-Controlled Crystal Oscillator.

� Centralized TDOA correction algorithm based on Reference

Transponder.

� Mode S transmitter with Whisper&Shout funcionality for Mode A/C

interrogations.

� Digital Signal Processing based on very high density FPGA with

common SoC solution for Receiving and Transmitting Stations.

� Dual Redundant Multilateration Processors based on Real Time

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� Dual Redundant Multilateration Processors based on Real Time

Operating System.


� Low number of LRUs.

� Simple Modular Design.

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s� Mode A/C/S MLAT system fully ED-117 and ICAO Annex 10 compliant.

� Interrogation, detection and acquisition in Modes 3/A, C, Mode S, extended

Summary


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� Interrogation, detection and acquisition in Modes 3/A, C, Mode S, extended squitter and short squitter.

� 100% Standards-based ADS-B redundant configuration. Complete ADS-B integration.

� Surface Multilateration with Mode S Enhanced Surveillance Functionality.

� Provides a Geographical situation of the vehicles independent of the avionics reports.

� Aircraft Identification, ICAO Address.

� High update rate with synchronous mode (1Hz).

� Able to work in asynchronous mode.

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� Able to work in asynchronous mode.

� Provides ASTERIX CAT 10, 19, 20, 21. (1, 2, 34, 48 and radar simulation with rotating sectors as option.)

� Automatic best receiving antenna selection.

� A-SMGCS integrated. With SMR radars, Data Fusion Equipment and Level 2 Safety Net

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DSPDSPDSP


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CORRELATIONCLOCK

CORRECTION

TOAsTR

COMMUNICATIONS

ERDSP

ERDSP

ERDSP

SINT

SCHEDULER

INT

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ECP

MULTILATERATION DEMODULATION

DECODIFICATION

ASTERIXTRACKING

TDOAs

OUTPUT

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INDRA EXPERIENCESMMS FOR LEBL BARCELONA

� Multilateration System fully ED-117 and ICAO

Annex 10 compliant.


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Annex 10 compliant.

� 2 Control and monitoring systems (local and

remote)

� 6 Reference transponder

� Total of 38 receiving stations.

� Redundant clock with NTP server

� 6 Interrogators

�(selective interrogation)

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�Receiver capability

� Optical fiber links

� Test transponders

� Redundant Central Processor

� Visual Radar 3000

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DETECTION AND DECODING

Coverage System extendable to coverage required. (typ):

20 NM range around the airport


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20 NM range around the airport

5000 ft height around the airport

Probability of detection (Pd) SSR: > 97%

Mode S: > 99%

Probability of Code Validation Mode 3/A ≥ 98%

Mode C : ≥ 96%

Mode S : ≥ 99,9%

Code Detection (output inm. Upon detection) Mode 3/A, C.

Not delivery of erroneous data.

Codes 7500, 7600, 7700.

Military Emergency Reply Train.

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Military Emergency Reply Train.

Military Identity Reply Train.

False codes validated Mode 3/A: < 0.1%

Mode C: < 0.1%

Mode S: < 10-6 (over any 5sec period per target)

False targets S < 10-4%

A/C <= 0,1%

Overall Jump Rate < 0,02%

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Horizontal Accuracy 3m on critical Areas.

10m standard deviation in airport surface

Update rate Between 1 and 15 seconds (configurable)

POSITIONAL ACCURACY, WORKLOAD AND AVAILABILITY


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Update rate Between 1 and 15 seconds (configurable)

Process Delay < 250ms

Workload 500 targets (mode S) + 100 (mode A/C)

Antennas Omnidirectional or any kind as necessary

Consumptions Receiver < 50W

Transmitter < 150W

Rack ECP < 2000W

MTTR < 20 min.

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MTTR < 20 min.

MTBF > 40.000 hours

Outdoor equipment Temperature -30ºC to 55 ºC

Relative Humidity 5% to 95%

Altitude 0 to 3600 m

Rain till 60 mm/hour

Perform Protection IP-67

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MAIN INTERFACES

ICAO DF/UF


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ASTERIX Cat. 10, 20, 21

PLOTS AND

TRACK

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ASTERIX Cat. 10, 20, 21

ATCC

ACC

TWR

TRACK

MANAGEMENT

STATUS

MANAGEMENT

PLOTS & TRACKS

STATUS

ASTERIX Cat. 19

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INDEX

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� En-Route, TMA and airport surface

surveillance applications

INDRA WAM SYSTEM

03 Indra WAM System – Product Overview

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surveillance applications

� High density traffic supported, process

more than 30.000 replies at each

receiver.

� Enhanced Surveillance performances

(ED-142)

� Co-operative with other

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� Co-operative with other

surveillance systems (Primary

radar, SSR, ADSB validation)

� Full solid-state technology

� Short term delivery and

commissioning

Sys

tem

s

Complete WAM Equipment, Communications and C&M System

WIDE AREA MULTILATERATION SYSTEM

ACCRECEIVING STATIONS

INTERROGATION STATIONS


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Communication Links

(Optical Fibre, Microwave, Modem, etc.)

RADAR MAINTENANCE

DISPLAY VR3000

REMOTE CONTROL AND


SRG SRG

CPS

TIME SUBSYSTEM

Recording

& analysis PC

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COMMUNICATIONS

SYSTEM (x2)

PRINTER

WAN(Ethernet)

LOCAL CONTROL AND


SLG SLG

Sys

tem

s


� Timestamp and synchronisation provided by common view GNSS

�


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� Dynamic cluster selection to obtain best possible solution in each situation.

� Two identical channels for redundancy and high MTBCF (more than 40,000

hours)

� Provides tracks in ASTERIX Cat019/020/021/23/247. Categories 1, 2, 34 and

48 as option.

� SNMP based control and monitoring system

� Positional detection by High update rate

� High degree of integration:

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� High degree of integration:

� COTS Power PC Processor

� High Pd in extreme SSR and Mode S Fruit Environments

� Powerful integrated BITE


� Simple Modular Design

Sys

tem

s

Interrogator ReceiverGPS antSSR ant

UPS

SSR ant

MHB

� Interrogation, detection and

acquisition in Modes 1, 2, 3/A, C,

Mode S and ES.

Main Functions


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ECP

GPS

receiverBITE

UPS

Mode S

transmitter

MHB

L band

receiver

COMMS

Interface

CAP

Module

INT Management

Whisper &

shout

PRF

management

ER Management

Dynamic

cluster

Want

list

BITE

COMMS

Interface

Mode S and ES.

� Adaptive Mode S Interrogation

schedule.

� Multi-ranging

� Full Mode S Enhanced

Surveillance functionality.

� ADS-B processing

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WAM & ADSB

Management

- Sync

- TDOA processing

- Correlator

- Locator

- Tracker

- Formatter

NTP server &

management

BITE

ASTERIX CAT 019, 023, 247

SNMPPAsterix CAT 20, 21

� ADS-B processing

� Optional ASTERIX categories 1,

2, 34 and 48

Sys

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s

Radar Coverage System extendable to coverage

Detection and Decoding


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Radar Coverage System extendable to coverage

required. Easy upgrade and

integration

Probability of detection (Pd) SSR: ≥≥≥≥ 97%

Mode S: ≥≥≥≥ 99%

Probability of Code Validation Mode 3/A ≥ 98 %

Mode C : ≥ 96 %

Mode S : ≥ 99,9 %


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Not delivery of erroneous data.

False codes validated Mode 3/A: < 0.1%

Mode C: < 0.1%

Sys

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sMaximal Positional Accuracy 3 m

Positional Accuracy


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Minimal Positional Accuracy 150 m

Positional Resolution (En-Route) >60% of Pd for two targets separated 2 Nm

>98% of Pd for two targets separated 4 Nm

Positional Resolution (TMA) >60% of Pd for two targets separated 0.6 Nm

>98% of Pd for two targets separated 2 Nm

Update period

Synchronous mode:

Update period is configurable between 1 and 15

seconds.

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Synchronous mode:

Asynchronous mode:

Standard synchronous periods:

seconds.

Position data age < 500ms

ASTERIX CAT 20 is generated after each position

decoding.

Position data age < 500ms

8 Seconds En-Route

5 Seconds TMA

Sys

tem

sTarget Load

Per Scan 600 targets

Workload and Availability


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Per Scan

Per Receiver

Want Lists

600 targets

Up to 30.000 replies / second

Used to prioritize requested replies

Processing delay < 500ms (excluding communications delay).

Minimization of Re-Interrogation Rate Absence of reply to a Comm-A interrogation, re-

interrogation with separated surveillance (UF4, 5)

and Comm-A Interrogations (UF20, 21)

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Useful Life Cycle 15 years

MTBCF > 40.000 hours

Availability > 99.999%

MTTR ≤≤≤≤ 20 min.

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WAM SYSTEM ARCHITECTURE

Full Redundant System

� Two identical

Interrogator WAM STATION ACC


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Interrogator

channels

� Two identical

LAN’s

� Two identical

Local Control and

Monitoring

Systems

� Two identical

Communication

Systems

� Two identical PERSONAL

COMPUTER

RADAR MAINTENANCE

DISPLAY VR3000

WAM STATION ACC

REMOTE CONTROL AND


SRG SRG

RECEIVER STATIONSINTERROGATION STATIONS

Communication Links

(Optical Fibre, Microwave, Modem, etc.)

TIME SUBSYSTEM

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� Two identical

Remote Control

and Monitoring

Systems

UPS

COMMUNICATIONS

SYSTEM (x2)

COMPUTER

PRINTER

DISPLAY VR3000

WAN(Ethernet)

LOCAL CONTROL AND


SLG SLG

ECPECP

Sys

tem

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INDEX

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SYSTEM BUILT-IN TEST

� Powerful BITE allows to detect 90% of failures in a single LRU and 95% of failures in two or more LRUs


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SRG Indication: SRG/SLG Indication: UCS Indication: LRU Indication:

95% of failures in two or more LRUs

� Graphical report of failures in all levels of Control and Monitoring applications using text and colour coded status elements.

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� All failures are reported and can be located from Local or Remote Control and Monitoring System

� Each channel provides BITE information Transmitter, Receiver, Pot Extractor and Communication Channels

SRG Indication:ADSB-GSS in failure

SRG/SLG Indication:ADSB-GSS in failure

UCS Indication:ADSB-GSS Slave

LRU Indication:TCPU module in

failure

Sys

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� Indra ASTTool� Recording, and visualization of system

ASTERIX Output Data.

� PPI type visualization

� Listing visualization

� Detailed target data visualization


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� Indra GDR Tool� Continuous data ASTERIX and

RAW recording

� Configurable size and schedule programming

� Indra Deployment Tool� Worldwide usable

� Configurable antenna parameters

�

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434343

� Number of receivers seen points in space

� Predicted horizontal and global errors (HDOP, GDOP)

Sys

tem

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� Eurocontrol RASS-R, RASS-S Tool

� Deep Analysis of system ASTERIX Output Data.

� System Performance Calculations

� Text and Graphical Results

� Integrity & sensibility testing


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� Integrity & sensibility testing

� ADS-B functionality Testing

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Sys

tem

s

� Deployment Tool

�Optimal Station Locations to meet coverage requirements.

� Configurable antenna

parameters


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parameters

� Number of receivers seen

points in space

� Predicted horizontal and

global errors (HDOP, GDOP)

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� Valid for Local and Wide area

deployments (including final

approach).

� Horizontal or oblique calculations

(final approach area).

Sys

tem

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INDEX

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Sys

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s

More than 30 years of experience on Surveillance Systems

WORLDWIDE CUSTOMERS OF INDRA ADS-B SYSTEMS


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� Some Indra ADS-B installations:

� 3x ADSB-GSS/22 + 1x ADSB-GSS/10 installed at Morocco

� 1x ADSB-GSS/20 installed at Saentis and Dübendorf

(Switzerland)

� 1x ADSB-GSS/20 installed at Barajas (Spain)

� 1x ADSB-GSS/20 installed at Tianjin(China)

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� 1x ADSB-GSS/20 installed at Tianjin(China)

� 2 Prototypes to be delivered for Eurocontrol and SESAR

projects.

Sys

tem

s

More than 30 years of experience on Surveillance Systems

� Sample MLAT/WAM Projects:

WORLDWIDE CUSTOMERS OF INDRA SURVEILLANCE SYSTEMS


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� Sample MLAT/WAM Projects:

� MLAT systems being deployed at Barcelona and Vilnius airports

(up to 6NM coverage)

� MLAT system being deployed at Latacunga airport (surface +

TMA) (up to 20NM coverage)

� WAM systems used for RVSM validation:

� Eurocontrol: Geneva (since 1998), Nattenheim (since 1998), Linz

(being deployed)

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(being deployed)

� NATS (since 1997)

� NAV CANADA (since 1996)

� WAM systems used for TMA and approach at ECUADOR.

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Indra’s ADS-B INSTALLATION SAMPLES

Barajas, Spain

Paracuellos, Spain


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Casablanca, Morocco

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Säntis, Switzerland

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WAM/MLAT INSTALLATIONS SAMPLES


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HME GenevaSouthampton

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Barcelona - SpainSwitzerland

Spain China - Xian Guatemala - La Aurora

HME Nattenheim

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INDEX

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WHAT IS Indra ATM? - SYSTEM MISSION

To enhance the safety of the flights by providing the controllerswith information of air movements from Surveillance Sensors suchas Radars, ADS B, Multilateration Systems and Weather Data,Planning information such as Flight Plans, Route Availability and


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Planning information such as Flight Plans, Route Availability andFlow Management and communicate control via Voice and DataLink

Aircon 2100 is one of the

most advanced, safest and

more reliable automated Air

Traffic Control System and in

a continuous evolution path.

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sa continuous evolution path.

Operating in over 50

countries worldwide,

integrating the latest & most

advanced ATC functionalities.

Sys

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� Incorporates the features derived from the

Eurocontrol studies (ODID III and IV) on HMI

(Human Machine Interface) for air traffic

controllers.

SDD - Design Characteristics


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controllers.

� Uses High Resolution Monitors (2Kx2K,

1600x1280, 1Kx1K).

� Integrates all information (radar, FP, DF, maps,

MET, ADS/CPDLC, etc) , able to be accessed

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MET, ADS/CPDLC, etc) , able to be accessed

selectively.

� Designed for both radar (executive) and

procedural controllers.

� Colors are used to distinguish flight’s ownership,

emphasize alarms, distinguish objects.

� User can configure desired colors, symbols, etc.

Sys

tem

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SDD - Track Display All tracks in RVSM alert condition (any non correlated track or any track correlated with a non RVSM equipped flight plan and located inside the RVSM airspace) aredistinguished by an special


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distinguished by an special alert.

Line 0: a) Assigned Sector

b) Distress indicator (HI, CO, EM, AD)

c) MSAW (MS) / MTCD (FP) / STCA (PR & VI) / RAW (OO & WI) indicators

Line 1: a) Callsign / ICAO SSR Code

b) Aircraft Type

Track label fields are totally off-line configured: in its situation

in label, in its colour and in its sensitive actions.

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sb) Aircraft Type

c) Turbulence

Line 2: a) Mode C Attitude (1 symbol : ↑or ↓ or space)

b) CFL level entered by the radar controller and CLAM alert indication

c) Lost indicator

d) Ground speed / vertical speed

Line 3: a) Heading

b) Assign Speed

c) Route Adherence Monitoring indicator (RAM)

d) ADES (Airport / Destination)

Line 4: Free textTRACK LABEL LINES

(example)

TRACK SYMBOLS

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tem

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SDD - ADS Information

ADS INFORMATION IN THE TRACK LABEL

� ADS capability/ ADS connection established indicators.

� CPDLC capability/ CPDLC connection established indicators.


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� CPDLC capability/ CPDLC connection established indicators.

� Navigation Integrity Control (NIC) Indicator.

� ADS Emergency mode indicator.

� Predicted Route (two next waypoints) from ADS, available.

� ADS event indicator: Whenever any of the requested events of the

ADS contract are fulfilled ,this circumstance is indicated until

acknowledged by the operator:

• Altitude Range (AR);

• Vertical Rate (VR);

• Lateral Deviation (LD);

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• Lateral Deviation (LD);

• Waypoint Change (WP).

OTHER ADS INFORMATION

• Position Reports;

• Next Waypoints (predicted route).

Sys

tem

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SDD - Predicted Route & Route Insertion

Error (RIE) Warning

� When the Predicted Route Group

information is available, the next two route

waypoints (received from the ADS or


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CPDLC) can be displayed.

�Clicking on the field “ADS predicted

route availability indicator” of tracks with

ADS information, the predicted route (next

two waypoints) is activated and

deactivated.

� If the route differs from the filled in the

FP, a RIE warning is issued (route in

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FP, a RIE warning is issued (route in

yellow color).

� Route insert error function (RIE) alerts

the controller when the planned routes

stored in ADS track received in ADS or

CPDLC reports, are different from ground

FP route.

Sys

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INDEX

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MEDIUM TERM

� ATCOs Workload will be reduced due to automatic verification

of actual Flight Plan (FP) against their calculated profiles.

� New parameters, such as fuel load, will be available for ACC

profile calculation. This information will be available to ATC


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profile calculation. This information will be available to ATC

Systems through Directed Interrogation Messages (ASTERIX

Cat. 7).

� Complete replacement of SSR by SSR Mode S.

� Technology mix to service areas with low radar coverage and

to have redundancy where needed (MSSR+ADS-B).

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Sys

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s


� SSR Mode S Radars will be deployed where circumstances will make

the cost-effective:

� Sites with good coverage and existing radar infrastructure.

� Sites with limited communications infrastructure.

LONG TERM

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� Sites with limited communications infrastructure.

� Sites where a Primary Radar (PSR) is needed.

� ADS-B will become more and more important for surveillance, due to

its cost-effectiveness.

� MLAT Technology, specially WAM, will become the alternative for

those areas where SSR is not viable, such as very mountainous

areas.

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Sys

tem

sim

ple

me

nta

tio

ns

. A

DS

B/W

AM

in

teg

rati

on

wit

hIn

dra

’sA

TC

Sys

tem

sA

DS

B,

WA

M,

ML

AT

im

ple

me

nta

tio

ns

61

Avda. de Bruselas 35

28108 Alcobendas,

Madrid España

T +34 91 480 50 00

F +34 91 480 50 80

www.indra.es

ATM International & Airports ADSB, WAM, MLAT ...Indra’sMODES TRANSPONDER Systems CONTROLER...

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Transcript of ATM International & Airports ADSB, WAM, MLAT ...Indra’sMODES TRANSPONDER Systems CONTROLER...