Intelligent proportional-derivative control for flexible spacecraft attitude stabilization with unknown input saturation

Engineering

• Stable State 100%
• Flexible Spacecraft 100%
• Derivative Control 100%
• Control Law 50%
• Control Scheme 50%
• Control Input 50%
• Gain Control 50%
• Radial Basis Function 25%
• Feedback Control 25%
• Parameter Uncertainty 25%
• Actuator 25%
• Nonlinearity 25%
• Attitude Control 25%
• Lyapunov Function 25%
• Closed Loop 25%
• Feedforward 25%
• External Disturbance 25%
• Initial Condition 25%
• Derivative Controller 25%
• Sufficient Condition 25%