Multi-Fidelity Modeling and Adaptive Co-Kriging-Based Optimization for All-Electric Geostationary Orbit Satellite Systems

Engineering

• Computational Cost 40%
• Demonstrates 20%
• Design System 40%
• Dynamic Models 20%
• Engineering 20%
• Finite Element Method 20%
• Geostationary Orbit 100%
• Model Element 20%
• Model Fidelity 40%
• Multidisciplinary Design Optimization 80%
• Optimisation Problem 80%
• Orbital Transfer 20%
• Sample Point 20%