Fault tolerant integrated radar/inertial altimeter based on Nonlinear Robust Adaptive Kalman filter

Keyphrases

• Fault-tolerant 100%
• Altimeter 100%
• Robust Adaptive Kalman Filter 100%
• Filter Gain 40%
• Posterior Probability 40%
• Noise Measurement 20%
• Estimation System 20%
• Current Measurement 20%
• Gain Correction 20%
• Innovation Sequence 20%
• Integrated Navigation System 20%
• Measurement Fault 20%
• Radar Altimeter 20%
• Open-loop System 20%
• Current Estimation 20%
• Filtration Algorithms 20%
• Posterior Probability Density 20%
• Weight Coefficient 20%
• Abnormal Measurements 20%
• Innovation Vector 20%

Engineering

• Kalman Filter 100%
• Posterior Probability 100%
• Measurement Noise 33%
• Loop Control System 33%
• Open Loop 33%
• Main Source 33%
• Continuous Measurement 33%
• Probability Density 33%
• Current Measurement 33%

Earth and Planetary Sciences

• Kalman Filter 100%
• Noise Measurement 50%
• Integrated Navigation 50%
• Radio Altimeter 50%