Spacecraft formation flying control under orbital perturbations by state-dependent Riccati equation method in the presence of on–off actuators

Keyphrases

• Spacecraft Formation Flying 100%
• Orbital Perturbations 100%
• Actuator 100%
• State-dependent Riccati Equation Technique 100%
• Controller 100%
• Formation Flying Control 100%
• Operating Conditions 50%
• Nonlinear Model 25%
• Nonlinear Problems 25%
• Controller Design 25%
• Motion Model 25%
• Leader-follower 25%
• Energy Consumption 25%
• Simple Controller 25%
• Real Conditions 25%
• Thruster 25%
• State-dependent Riccati Equation 25%
• Continuous Signals 25%
• Pulse-width Pulse-frequency Modulator 25%

Engineering

• Riccati Equation 100%
• Operational Condition 66%
• Nonlinear Problem 33%
• Pulse Frequency 33%
• Nonlinear Model 33%
• Controller Design 33%
• Thruster 33%
• Pulse Duration 33%
• Energy Engineering 33%
• Continuous Signal 33%