Optimal formation keeping near a general keplerian orbit under nonlinear perturbations

Engineering

• Nonlinearity 66%
• Applicability 33%
• Analytics 33%
• Reference Trajectory 33%
• Hamiltonian 33%
• Finite Time 33%
• Numerical Experiment 33%
• Control Logic 33%
• Cost Reduction 33%
• Inertial Frame 33%
• Propulsion System 33%
• Coordinate Transformation 33%
• High Precision 33%
• Design 33%
• Complexity 33%
• Demonstrates 33%
• Accuracy 33%
• Coordinate 33%
• Spacecraft 33%

Physics

• Tracking 100%
• Feedback Control 33%
• Keplerian Orbit 33%
• Shapes 33%
• Coordinates 33%
• Earth 33%