Safety-Critical Attitude Tracking of Spacecraft With Data-Based Parameter Identification

Engineering

• Adaptive Hybrid 50%
• Angular Velocity ω 50%
• Barrier Function 50%
• Binary Logic 50%
• Control Strategy 100%
• Error Estimate 50%
• Excitation Condition 50%
• Feedback Control 50%
• Selection Criterion 50%
• Simulation Result 50%

Computer Science

• Angular Velocity 50%
• Critical Attitude 100%