Equations of motion for maneuvering flexible spacecraft

DOI10.2514/3.20240zbMath0634.70026OpenAlexW2170727232MaRDI QIDQ3773439

Roger D. Quinn, L. Meirovitch

Publication date: 1987

Published in: Journal of Guidance, Control, and Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.20240

zbMATH Keywords

small elastic deformationsperturbation approachlarge rigid-body maneuversmaneuver force distributionmaneuvering flexible spacecraft

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Kinematics of mechanisms and robots (70B15) Orbital mechanics (70M20)

Related Items (8)

Variational approaches for dynamics and time-finite-elements: Numerical studies ⋮ Dynamics and stabilization of a flexible orbiting spacecraft with a rigid tip body ⋮ Математическая модель спутника с произвольным числом нежестких элементов ⋮ Multibody Dynamics and Nonlinear Control of Flexible Space Structures ⋮ Methods for the vibration determination and parameter identification of spacecraft with flexible structures ⋮ Coupling dynamic analysis of spacecraft with multiple cylindrical tanks and flexible appendages ⋮ Optimal vibration control of flexible spacecraft during a minimum-time maneuver ⋮ A general formulation for the nonlinear dynamics and control of orbiting flexible structures

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