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Potential ATS Ground Surveillance Configuration
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同源图形
Relationship Between
Functional Relations
ATS Ground Surveilla
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:
Update Period Requir
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
相关图形
ATS 组成框图
GJB 5937-2007
军用电子装备自动测试
图 1 ATS 的体系结构
GJB 7248-2011
自动测试系统体系结构
图 6 ATS 内部各功能
GJB 7248-2011
自动测试系统体系结构
Landing Gear Configu
AIR1489B
Aerospace
Boeing 767 Forward L
AIR1673A
Aircraft C
Tristar Lower Hold C
AIR1673A
Aircraft C
FIGURE 11 - GROUND T
AIR1678B
Uncertaint
GROUND TEST MEASUREM
AIR1678B
Uncertaint
Plenum Configuration
AIR1826
Acoustical
Conventional Rip-Sto
AIR4002
8000 psi H