Coupled orbit-attitude dynamics of tethered-SPS
From MaRDI portal
Publication:2004135
DOI10.1155/2020/6721301zbMath1459.70046OpenAlexW3088082416MaRDI QIDQ2004135
Publication date: 14 October 2020
Published in: Mathematical Problems in Engineering (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1155/2020/6721301
Multistep, Runge-Kutta and extrapolation methods for ordinary differential equations (65L06) Orbital mechanics (70M20)
Cites Work
- Projected Runge-Kutta methods for constrained Hamiltonian systems
- Efficient implementation of symplectic implicit Runge-Kutta schemes with simplified Newton iterations
- Strategy for sensor number determination and placement optimization with incomplete information based on interval possibility model and clustering avoidance distribution index
- Vibration and elastic wave propagation in spatial flexible damping panel attached to four special springs
- Symplectic algorithms based on the principle of least action and generating functions
- Symplectic Geometric Algorithms for Hamiltonian Systems
- Dynamics of Multibody Systems
- Long-term dynamic modeling of tethered spacecraft using nodal position finite element method and symplectic integration
