Relative Attitude-orbit Coupling Proximity Control for Underactuated Small Spacecraft

Engineering

• Control Vector 100%
• Actuator 50%
• Degree of Freedom 50%
• Finite-Time Stability 50%
• Sliding Mode Control 50%
• Sliding Mode 50%
• Dynamic Model 50%
• Model Uncertainty 50%
• Control Input 50%
• Freedom System 50%
• Lyapunov Stability 50%