Attitude dynamics of a liquid-filled spacecraft with a manipulator

DOI10.1016/S1007-5704(97)90033-2zbMath0936.70025MaRDI QIDQ1289753

Zhao-Lin Wang, Jun-Feng Li

Publication date: 28 July 1999

Published in: Communications in Nonlinear Science and Numerical Simulation (Search for Journal in Brave)

zbMATH Keywords

space manipulatorattitude stability of spacecraftcoordinate manipulators operationlaw of joint anglesoperation time

Mathematics Subject Classification ID

Incompressible viscous fluids (76D99) Orbital mechanics (70M20)

Related Items (4)

Analytical method for the attitude stability of partially liquid filled spacecraft with flexible appendage ⋮ Attitude stabilization of rigid spacecraft with disturbance generated by time varying uncertain exosystems ⋮ Modeling and numerical simulation of linear and nonlinear spacecraft attitude dynamics and gravity gradient moments: a comparative study ⋮ Attitude control of rigid spacecraft with disturbance generated by time varying exosystems

Cites Work

• Reorientation of a structure in space using a three-link rigid manipulator

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