Development and verification of a flexible tethered satellite system model considering the fuel slosh

DOI10.1007/S11044-022-09845-WzbMath1505.70054OpenAlexW4296966001MaRDI QIDQ2099669

Zahra Jafari Shahbazzadeh, Ramin Vatankhah, Mohammad Eghtesad, Nima Assadian

Publication date: 24 November 2022

Published in: Multibody System Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11044-022-09845-w

zbMATH Keywords

parametric studytethered satellitedynamic modellingMATLAB simulatormodified Lagrange methodNX Siemens software

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Orbital mechanics (70M20) Dynamics of multibody systems (70E55)

Related Items (1)

Out-of-plane chaotic motion and suppression for tethered tug-debris systems with thrust perturbation

Uses Software

• Matlab
• NX

Cites Work

• Dynamics and control of a smart flexible satellite moving in an orbit
• Thrust vector control of an upper-stage rocket with multiple propellant slosh modes
• Integrated vibration suppression attitude control for flexible spacecrafts with internal liquid sloshing
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