Spacecraft angular rate estimation from vector observations using a fast particle filter

Keyphrases

• Fast Particles 100%
• Particle Filter 100%
• Vector Observations 100%
• Angular Velocity Estimation 100%
• Inertia Tensor 66%
• Maximum Likelihood Estimation 33%
• Monte Carlo 33%
• Particle number 33%
• High Efficiency 33%
• Time Propagation 33%
• Numerical Representation 33%
• Sequential Method 33%
• Novel Algorithm 33%
• Simulation Study 33%
• Extended Kalman Filter 33%
• Time Measurement 33%
• Additional Filter 33%
• Non-Gaussian Probability Density Function 33%
• Representation Technique 33%
• Three-axis Magnetometer 33%
• Inherently Nonlinear Systems 33%
• Measurement Update 33%
• Geomagnetic Field Measurement 33%
• Low Earth Orbit 33%
• Fast Convergence Rate 33%
• Angular Rate 33%

Engineering

• Observation Vector 100%
• Particle Filter 100%
• Gaussians 33%
• Nonlinear System 33%
• Convergence Rate 33%
• Probability Density Function 33%
• Extended Kalman Filter 33%
• Low Earth Orbit 33%
• Field Measurement 33%
• Maximum Likelihood Estimate 33%
• Inertia Tensor 33%
• Filter State 33%