Spacecraft attitude estimation via stochastic H _∞ filtering

Keyphrases

• Spacecraft Attitude Estimation 100%
• H Filtering 100%
• Estimation Error 60%
• Kalman Filter 60%
• Monte Carlo 40%
• Noise Level 40%
• Quaternion 40%
• Attitude Quaternion 40%
• Quaternion Kalman Filter 40%
• Gyro 40%
• Noise Intensity 40%
• Disturbance Attenuation 40%
• Line-of-sight 20%
• Monte Carlo Simulation 20%
• Stochastic Processes 20%
• Noise Free 20%
• Per Se 20%
• Low Noise 20%
• Spacecraft Attitude 20%
• Attitude Estimation 20%
• Unknown Variance 20%
• Line-of-sight Measurement 20%
• Noise Covariance 20%
• Attitude Sensing 20%
• Filter Gain 20%
• Variance Parameter 20%
• Transmission Gain 20%
• Differential Set 20%
• Differential Linear Matrix Inequality 20%
• Anticipative 20%

Engineering

• Filtration 100%
• Kalman Filter 100%
• Estimation Error 60%
• Intensity Noise 40%
• White Noise 40%
• Transmissions 20%
• Noise Level 20%