terrain and traffic collision avoidance system t 2 cas - the second generation taws
DESCRIPTION
Terrain and Traffic Collision Avoidance System T 2 CAS - The second generation TAWS. Thales group : A worldwide leader. Aerospace. Air Systems. Land & Joint Systems. Services. Naval. Security. 2005 Sales: €10.3bn - Order book: €20.2bn. 60,000 employees in 50 countries. - PowerPoint PPT PresentationTRANSCRIPT
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2005 Sales: €10.3bn - Order book: €20.2bn
Land & JointSystems
Air Systems
Aerospace Naval
60,000 employees in 50 countries
Security Services
Thales group : A worldwide leader
A worldwide leader in both civil and defence marketsA worldwide leader in both civil and defence markets
3
THALES MARS SIMULATION
Avionics functionFM, Taxi, TAWS, TCAS..
Aircraft Model
EnvironmentdB server
Traffic gene.Atmo. Gene.
Ground
ATC p
ositio
nAirp
ort o
pera
tion
AOC* p
ositio
n
ATC position consists of an
EUROCAT station
Unique Market Position to integrate Air and Ground solutionsUnique Market Position to integrate Air and Ground solutions
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THALES Aerospace: brief history
JAEGER
BADINCROUZET
SFENAEAS THOMSON-CSF/AVG
SEXTANT AVIONIQUE 1989
THOMSON-CSF SEXTANT 1999
L-3 Communications (JV) ACSS
VDO+BGT (JV) Diehl Avionik Systeme GmbH
Racal Thales Avionics Ltd
Thales Avionics- Inflight Systems
Auxilec Thales Avionics Electrical Systems
2000
2001
1999
2000
MORS
Thales Aerospace Division2004 THALES Airborne Systems
B/E Aerospace
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What is T²CAS?
TCAS 2000 = Proven Second Generation TCAS system with TCAS 2000 = Proven Second Generation TCAS system with over 9000 units flyingover 9000 units flying
Certified Certified TAWS: GCAM = second generation TAWSTAWS: GCAM = second generation TAWS
Enhanced TAWS and Proven TCAS combinedEnhanced TAWS and Proven TCAS combined
Reduced LRU count
Second generation TAWS :
Performance based Sensors
Enhanced Landing Protection
Lower cost of ownership
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Performance Based Clearance Sensors
Digital Terrain DatabaseDigital Terrain Database
WARNIN
G
WARNIN
G
8 Sec.
112 s
GPS
CAUTION
CAUTION
20 Sec.
Respond
Climb CapabilityReact
112 s
At all time …
The short-term segment of the clearance sensor models what the aircraft is currently doing: True current flight path angle
The long-term segment of the clearance sensor models what the aircraft could do if an alert were to occur: Actual climb performance
As compared to conventional clearance sensors, this allows a longer clearance sensor to be built without generating nuisance alerts.
Performance Based Alerts , enhancing safetyPerformance Based Alerts , enhancing safety
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T2CAS Runway Convergence Envelope Overview
Figure 1 TAWS Convergence Envelope: Inhibition When Landing Normally, Alerting Enabled When Outside of Normal Landing Area
Runway
2.64º
0.3 Nm
8º
Inhibition Region
Non - Inhibition
Non - InhibitionCross-section:
The T2CAS provides CFIT (Controlled Flight Into Terrain) protection for all phases of flight, including the approach and landing phase. The Convergence Envelope (or “Landing Tunnel”) logic is designed to predict whether the aircraft is properly converging on the runway for a safe landing. If proper convergence is predicted, the forward-looking Collision Predicting and Alerting (CPA) function is inhibited (the reactive GPWS modes remain active throughout the landing procedure).
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T2CAS Runway Convergence Envelope Overview
The Convergence Envelope is NOT simply a volume of space within which CPA alerting is inhibited. The previous figure above (reproduced from the ACSS T2CAS Pilot’s Guide, Doc 8000264-001 Rev 1) loosely illustrates the physical geometry of the Convergence Envelope in terms of:
Distance from Runway
Vertical Position
Horizontal Position
However, landing tunnel does also include these additional conditions:
Track Angle
Vertical Speed
Flap and Gear Setting – one of the two must be down to inhibit
Runway position accuracy is essentialRunway position accuracy is essential
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T2CAS Runway Convergence Envelope Overview
In summary, the T2CAS TAWS function inhibits CPA alerting during runway approaches as long as the following conditions are met:
Aircraft is in Approach Phase Aircraft is in proper Landing Configuration Runway Convergence is predicted The CPA function can be re-enabled at any time if these
conditions fail to remain satisfied. At this point the system will generate the appropriate alerts, should a CFIT potential exist.
Runway
2.64º
0.3 Nm
Inhibition Region
Non - Inhibition
Alert Possible!
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T2CAS Runway Convergence Envelope Overview
If Runway Source Data is in error, nuisance alerts can result.
Example of Runway Threshold Location Problem at ONE AIRPORT Which Causes a Misaligned Tunnel and Nuisance Alert
Initial source data shows westward
lateral shift of 0.5
Nm
Initial source data shows westward
lateral shift of 0.5
Nm
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T2CAS Runway Convergence Envelope Overview
DB 20 Misaligned Tunnel Causes a Nuisance Alert to be Indicated
Inhibition on Horizontal Position
28.79
28.81
28.83
28.85
28.87
28.89
28.91
115.79 115.84 115.89 115.94 115.99
Longitude
Latit
ude
Horizontal Landing Tunnel
Runway
Flightpath
DB20 Runway Threshold is defined to the left of the actual runway. The Aircraft Exits the Horizontal Landing Tunnel and an alert is indicated via CPA sensor contacting the “terrain” of the runway.
XX.91
XX.89
XX.87
XX.85
XX.83
XX.81
XX.79
XX5.79 XX5.84 XX5.89 XX5.94 XX5.99
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T2CAS Runway Convergence Envelope Overview
DB 21 Corrects the Runway Location which Aligns the Tunnel. No Nuisance Alert Is Indicated.
Inhibition on Horizontal Position
28.79
28.81
28.83
28.85
28.87
28.89
28.91
115.80 115.85 115.90 115.95 116.00
Longitude
Latit
ude
Horizontal Landing Tunnel
Runway
Flightpath
DB21 Corrects the runway Threshold location. The Aircraft does not Exit the Horizontal Landing Tunnel and an alert is NOT indicated.
XX.91
XX.89
XX.87
XX.85
XX.83
XX.81
XX.79
XX5.79 XX5.84 XX5.89 XX5.94 XX5.99
Runway position accuracy is essentialRunway position accuracy is essential
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GPSGPS
CautionCaution - Aural Alert- Aural Alert Pull-UpPull-Up - Aural Warning- Aural Warning
WARNIN
G
WARNIN
G
CAUTION
CAUTION
112 112 SecondsSeconds
112 112 SecondsSeconds
CCurrent Climb Capability of Aircrafturrent Climb Capability of AircraftCCurrent Climb Capability of Aircrafturrent Climb Capability of Aircraft
Full Descent / Climb Path ProtectionFull Descent / Climb Path ProtectionFull Descent / Climb Path ProtectionFull Descent / Climb Path Protection
Terrain Adv. Line Advisory added to DisplayTerrain Adv. Line Advisory added to DisplayTerrain Adv. Line Advisory added to DisplayTerrain Adv. Line Advisory added to Display
Terrain Advisory LineTerrain Advisory Line –– Advisory Advisory
NewNew
‘‘AVOID’ when PULL-UP is NOT EnoughAVOID’ when PULL-UP is NOT Enough ‘‘AVOID’ when PULL-UP is NOT EnoughAVOID’ when PULL-UP is NOT Enough
AvoidAvoid - Aural Warning- Aural Warning
NewNew
Expanded Look when Entering TurnsExpanded Look when Entering Turns Expanded Look when Entering TurnsExpanded Look when Entering Turns
4-D Approach Projection for Landin4-D Approach Projection for Landingg 4-D Approach Projection for Landin4-D Approach Projection for Landingg
A broader Alert sequence to avoid accidents
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Database Development Process
AIS
EAG
THAV ACSS End-user
CivilAviation
Authorities
Terrain DataProviders
Terrain Data
Nav Data
Combined Data
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Terrain Data
•Source data comes from Official Terrain Data Providers US Geological Survey National Imaging and Mapping Agency Shuttle Radar Topographical Mission
(SRTM) Data Etc.
•Advanced InfoData Systems, GmbH (AIS) compiles the data Per DO-200a process
AIS
Terrain DataProviders
Terrain Data
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Airport and Runway Data
•Source data comes from Official State Agencies FAA/NACO JAA Etc.
•European Aeronautical Group (EAG) Generates an ARINC 424 database Per DO-200a process
EAG
CivilAviation
Authorities
Nav Data
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Combined Data
•Thales Avionics performs verification and validation of the data, filters the airport data, and merges Terrain and Airport Data into a single file Per DO-200a process Calculates 32bit CRC for integrity
checking
•ACSS attaches a file header and distributes the data to customers
THAV End-user
Combined Data
ACSS