Statistical confidence domain data driven based fast in-flight alignment method

Engineering

• Measurement Noise 100%
• Supports 50%
• Simulation Result 50%
• Test Result 50%
• State Variable 50%
• Kalman Filter 50%
• Inertial Navigation System 50%
• Additive Noise 50%
• Estimation Result 50%
• Non-Gaussian Noise 50%
• Flight Dynamics 50%
• Inertial Sensor 50%

Physics

• Noise Measurement 100%
• Non-Gaussian Noise 50%

Computer Science

• Statistical Confidence 100%