Attitude estimation of the Delfi-n3Xt satellite

Keyphrases

• Attitude Estimation 100%
• Sun Vector 100%
• Magnetic Field 20%
• Experimental Validation 20%
• Monte Carlo Simulation 20%
• Physical Parameters 20%
• Photodiode 20%
• SIMPLE Algorithm 20%
• Four-quadrant 20%
• Matrix-based 20%
• Dynamic Environment 20%
• Nanosatellite 20%
• Measurement Update 20%
• Body-mounted 20%
• Tumbling 20%
• Simulation Validation 20%
• Error Analysis 20%
• Order Reduction 20%
• Model Reduction 20%
• Line-of-sight Measurement 20%
• Process Noise 20%
• Quaternion Filter 20%
• Rank Deficiency 20%
• Albedo Effect 20%
• Sun Sensor 20%
• Rate Gyro 20%
• Earth Albedo 20%
• Covariance Propagation 20%
• TU Delft 20%
• Carlo Simulation 20%
• Multiplicative Process 20%
• Geometric Imperfection 20%
• Determination Algorithm 20%

Physics

• Spacecraft 100%
• Line of Sight 50%
• Monte Carlo Simulation 50%
• Photodiode 50%
• Defects 50%
• Covariance 50%
• Solar Sensor 50%
• Error Analysis 50%
• Earth Albedo 50%

Engineering

• Good Performance 100%
• Illustrates 50%
• Physical Parameter 50%
• Photodiode 50%
• Model Reduction 50%
• Nanosatellites 50%
• Process Noise 50%
• Rate Gyro 50%
• Albedo Effect 50%