Vector observations-based gyroless spacecraft attitude/angular rate estimation using particle filtering

Keyphrases

• Particle number 100%
• Spacecraft Attitude 100%
• Additional Filter 100%
• Vector Observations 100%
• Angular Velocity Estimation 100%
• Particle Filtering 100%
• Observation-driven 100%
• Gyroless Spacecraft 100%
• Monte Carlo 50%
• High Efficiency 50%
• Time Propagation 50%
• Numerical Representation 50%
• Sequential Method 50%
• Novel Algorithm 50%
• Filter Method 50%
• Simulation Study 50%
• Time Measurement 50%
• Non-Gaussian Probability Density Function 50%
• Unscented Kalman Filter 50%
• Representation Technique 50%
• Particle Filter 50%
• Three-axis Magnetometer 50%
• Inherently Nonlinear Systems 50%
• Measurement Update 50%
• Geomagnetic Field Measurement 50%
• Low Earth Orbit 50%
• Fast Convergence Rate 50%
• Angular Rate 50%
• Innovative Procedures 50%
• Curse of Dimensionality 50%

Engineering

• Filtration 100%
• Observation Vector 100%
• Gaussians 50%
• Dimensionality 50%
• Nonlinear System 50%
• Convergence Rate 50%
• Probability Density Function 50%
• Kalman Filter 50%
• Low Earth Orbit 50%
• Field Measurement 50%
• Particle Filter 50%