Long-term coupling effects between librational and orbital motions of a satellite
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Publication:5729788
DOI10.2514/3.2378zbMath0118.40507OpenAlexW1996924107MaRDI QIDQ5729788
Publication date: 1964
Published in: AIAA Journal (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.2514/3.2378
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Mathematical modelling and stabilization of large flexible spacecraft subject to orbital perturbation ⋮ Control of tethered satellite systems using thruster and offset strategies ⋮ Periodic Solutions and Controls of Tethered Systems in Elliptic Orbits ⋮ Dynamics and Control of Spinning Tethers for Rendezvous in Elliptic Orbits ⋮ The influence of satellite flexibility on orbital motion ⋮ A general formulation for the nonlinear dynamics and control of orbiting flexible structures ⋮ Controlled Dynamics of Flexible Orbiting Tethered Systems: Analysis and Experiments
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