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Update Period Requirements Analysis
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Relationship Between
Functional Relations
ATS Ground Surveilla
Potential ATS Ground
Position Reference P
Current TCP Informat
Current TCP,As Conve
Air-To-Air Capabilit
Relationship of MASP
Illustrative ADS-B S
ADS-B Subsystem Leve
ADS-B Functional Lev
Example of A/C Pair
Example of A/C Pair
Example of ADS-B Sup
Peak Traffic Based o
GNSS/ADS-B Surveilla
Meaning of Fields fo
Meaning of Fields fo
Meaning of Fields fo
Functional Relations
The ITC Concept as C
Illustration of the
Latitude Standard De
Incremental Increase
Implications of Full
Multipath Relationsh
Smooth EarthReflecti
Typical AircraftAnte
Air-Ground Relative
Air-Air Multipath Le
Air-Air Multipath Le
Air-Air Multipath De
Encounter Dynamic Re
Crossing Encounter w
Crossing Encounter w
Constant Alert Cover
Normalized Compariso
Comparison of Compos
Half Beamwidth Varia
Relative Gain of Mat
Barometric Pressure
Altitude Conflict Sc
Monte Carlo Simulati
Profile of Typical B
Use of Bank Angle/Tu
Use of Bank Angle/Tu
Latency and latency
Example of the Effec
Acceptable Surveilla
Future Collision Avo
Collision Avoidance
Collision Avoidance:
Altitude Conflict Sc
Altitude Conflict: W
Scenarios Used to As
Sensitivity to Error
Advisory Rate, US Da
1 Delayed Alert Rate
Free Flight Conflict
Free Flight Conflict
Free Flight Conflict
Free Flight–False Al
Free Flight–False Al
Free Flight False Al
Update Period Requir
1,000 ft Independent
1,000 ft Independent
1,000 ft Independent
1,000 ft Independent
1k ft Independent Pa
2,500 ft Independent
2,500 ft Independent
2,500 ft Independent
Update Period Requir
Update Period Requir
Scenario for Analysi
Simulation Results f
Simulation Results f
Surface Scenario 2-B
Accordion Concept
Separation vs. Time
Range at Which Braki
False Alarm Rates, 1
Required Received Re
Runway Incursion War
Relationship between
Example: Horizontal
Probability of Updat
Required Probability
Probability of Acqui
Probability of Acqui
TS Report and TC Rep
Aircraft Control Sta
Constant Vertical Sp
Intercept Course to
FMS Descent with Int
FMS Descent with MCP
Radius to Fix Turn
Fly-by Turn