An energy-matching optimal control method for consensus of spacecraft cluster flight

Engineering

• Optimal Control 100%
• Feedback Control 66%
• Relative Motion 66%
• Control Law 33%
• Dynamic Model 33%
• State Error 33%
• Initial Condition 33%
• Agent System 33%
• State Variable 33%
• Error Dynamic 33%
• Gain Matrix 33%
• Matching Condition 33%
• Semimajor Axis 33%

Physics

• Optimal Control 100%
• Spacecraft 100%
• Feedback Control 16%
• Synchronism 8%
• Semimajor Axis 8%
• Linear Quadratic Regulator 8%