Deployment and attitude control of a tethered subsatellite with controllable arm

Engineering

• Feedback Control System 100%
• Control Law 100%
• Open Loop 100%
• Attitude Control 100%
• Demonstrates 50%
• Main Step 50%
• Actuation 50%
• Optimal Control 50%
• Optimal Control Problem 50%
• Reference Trajectory 50%
• Control Constraint 50%
• Plane Motion 50%
• Open Loop Control 50%
• Momentum Wheel 50%