On novel appointed-time inertia-free adaptive attitude control of spacecraft

Engineering

• Attitude Control 100%
• Control Scheme 100%
• Convergence Time 100%
• External Disturbance 50%
• Finite Time 50%
• Output Feedback 50%
• Performance Function 50%
• Power State 50%
• Prescribed Performance 50%
• Sliding Mode Control 50%
• State Feedback 50%

Computer Science

• Appointed Time 100%
• Attitude-Controller 50%
• Output Feedback 50%
• Performance Function 50%
• Sliding Mode Control 50%
• State Feedback 50%
• Tracking State 50%