A Fault Detection and Isolation Design for a Dual Pitot Tube Air Data System

Keyphrases

• Detector Design 100%
• Air Data System 100%
• Fault Detection 100%
• Pitot Tube 100%
• Fault Isolation 100%
• Isolation Design 100%
• Detection Efficiency 50%
• Synthetic Air 50%
• Residual Test 50%
• Air Data 50%
• Air Speed 50%
• Protection Level 50%
• Inertial Measurement Unit 50%
• Global Navigation Satellite System Receiver 50%
• Data Fault Detection 50%
• Safety-critical 25%
• Unmanned Aerial Systems 25%
• Systems Approach 25%
• Threshold Method 25%
• Fault Detection Algorithm 25%
• Test Statistic 25%
• Angle of Attack 25%
• Observability Matrix 25%
• External Disturbances 25%
• Mathematical Derivation 25%
• System Work 25%
• Sideslip 25%
• Steady-state Error 25%
• Integrated Navigation System 25%
• Tube Failure 25%
• Sliding Window Size 25%
• Decision Logic 25%

Engineering

• Pitot-Tube 100%
• Units of Measurement 50%
• Inertial Measurement 50%
• Observability 25%
• Angle-of-Attack 25%
• Detection Algorithm 25%
• Navigation System 25%
• External Disturbance 25%
• State Error 25%
• Decision Logic 25%
• Test Statistic 25%