A finite element based stability test for equilibria of flexible structures in circular orbits

Keyphrases

• Finite Element 100%
• Element-by-element 100%
• Stability Test 100%
• Circular Orbits 100%
• Flexible Structure 100%
• Computational Effort 50%
• Finite Element Analysis 50%
• Energy Reduction 50%
• Earth Surface 50%
• Cyclic Coordinates 50%
• Energy-momentum Method 50%
• Eigenvector 50%
• Angular Momentum 50%
• Angular Rate 50%
• Space Elevator 50%
• Space Technology 50%
• Few Eigenvalues 50%
• Large Flexible Structure 50%
• System Dimensions 50%
• Tangent Stiffness Matrix 50%
• Overall Stability Analysis 50%
• Astronaut 50%
• Circular Motion 50%
• Celestial Body 50%
• Space Structure 50%
• Second Variation 50%
• Geostationary Orbit 50%
• Orbital Radii 50%
• Dirichlet 50%

Engineering

• Flexible Structures 100%
• Stability Test 100%
• Circular Orbit 100%
• Eigenvalue 50%
• Computational Effort 50%
• Stability Analysis 50%
• Angular Momentum 50%
• Elevators 50%
• Dirichlet 50%
• Celestial Body 50%
• Geostationary Orbit 50%
• Circular Motion 50%
• Stiffness Matrix 50%
• Eigenvector 50%

Mathematics

• Matrix (Mathematics) 100%
• Eigenvalue 100%
• Computational Effort 100%
• Stability Analysis 100%
• Angular Momentum 100%
• Circular Orbit 100%
• Tangent Stiffness 100%
• Eigenvector 100%