Design and verification of the state recovery controller for a drag-free satellite with two test masses

Engineering

• Buckingham's Theorem 50%
• Control System 50%
• Controller Design 50%
• Degree of Freedom 50%
• Design Parameter 50%
• Ground Simulation 100%
• Microgravity Environment 50%
• Platform Motion 50%
• Prevent Collision 50%
• Relative Distance 50%
• Scheme Design 50%
• Simulation Platform 100%
• Simulation Result 50%