Analysis of Dynamics and Control During the Deployment of an Annular Tether Group of Spacecraft

Engineering

• Complete Model 100%
• Control System 50%
• Coordinate System 50%
• Extensibility 50%
• Initial Condition 50%
• Lagrange Equation 50%
• Motion System 50%
• Numerical Example 50%
• Solid Body 50%
• Space Vehicle 50%