Keyphrases
Advanced Receiver Autonomous Integrity Monitoring (ARAIM)
86%
Global Navigation Satellite System
52%
Receiver Autonomous Integrity Monitoring
50%
Ground Based Augmentation System
40%
Fault Detection
39%
Dual Frequency
37%
Advanced RAIM
37%
Ionospheric Anomalies
37%
Service Type
31%
Civil Aviation
27%
Fault Exclusion
27%
Code-carrier Divergence
25%
Multiple Hypothesis Solution Separation
25%
Monitoring Method
25%
Elliptical Orbit
25%
Satellite Coverage
25%
Low Latitude
25%
Eigenvalue-based Detection
25%
Integrity Monitoring
21%
Ranging Error
21%
Separation Techniques
20%
J2 Perturbation
18%
BDS-3
18%
China
18%
Integrity Risk
18%
Carrier Phase
18%
Position Domain
18%
Vertical Protection Level
17%
Positioning Method
17%
LPV-200
17%
Test Statistic
16%
Baseline Length
15%
Satellite Constellation
15%
Single Satellite
15%
Horizontal Protection Level
15%
Positioning Application
13%
Test Metrics
12%
Resolution Method
12%
Weak Geometry
12%
Teardrop
12%
Relative Positioning
12%
Coverage Prediction
12%
Ambiguity Resolution
12%
System Time Offset
12%
Time Offset
12%
2D Map
12%
Observational Method
12%
Coverage Analysis
12%
Occlusion
12%
Field Mapping
12%
Engineering
Integrity Monitoring
100%
Augmentation System
56%
Service Type
37%
Test Statistic
34%
Carrier Phase
32%
Missed Detection
31%
Civil Aviation
31%
Solution Hypothesis
29%
Simulation Result
26%
Elliptical Orbit
25%
Critical Application
25%
Global Positioning System
23%
Service Availability
12%
Relative Positioning
12%
Spatial Correlation
12%
Stochastic Model
12%
Control Systems
12%
Space Method
12%
Network System
12%
Detection Probability
12%
Applied Technology
12%
Relative Motion
12%
Random Error
12%
Model Uncertainty
12%
Preliminary Design
12%
Reference Orbit
12%
Performance Standard
12%
Tangent Line
12%
Orbital Element
12%
Observables
12%
Computation Time
12%
State Transition Matrix
12%
Navigation System
12%
Core Technology
12%
Failure Rate
12%
Mathematical Model
12%
Computational Efficiency
10%
Metrics
10%
Gross Error
8%
Ground Target
8%
Constraint Function
8%
Error Performance
6%
Normal Distribution
6%
Position Error
6%
Selection Method
6%
Error Term
6%
Parallel Line
6%
Limitations
6%
Experimental Result
6%
Ascending Node
6%