Nonlinear observability analysis of spacecraft attitude and angular rate with inertia uncertainty

Keyphrases

• Spacecraft Attitude 100%
• Angular Rate 100%
• Inertia Uncertainty 100%
• Nonlinear Observability Analysis 100%
• Inertia 50%
• Inertia Tensor 50%
• Any Order 25%
• Control Input 25%
• Grid Filter 25%
• Nonlinear System Theory 25%
• Bayesian Grid 25%
• Unobservability 25%
• Momentum Wheel 25%
• Lie Derivative 25%
• Tensor Uncertainty 25%

Engineering

• Observability 100%
• Sufficient Condition 50%
• Observables 50%
• Inertia Tensor 50%
• Nonlinear System 25%
• Momentum Wheel 25%
• Control Input 25%
• Expression System 25%