Dual-quaternion-based adaptive motion tracking of spacecraft with reduced control effort

DOI10.1007/S11071-015-2350-4zbMath1349.93214OpenAlexW1247368940MaRDI QIDQ331254

George Vukovich, Hai-Chao Gui

Publication date: 26 October 2016

Published in: Nonlinear Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11071-015-2350-4

zbMATH Keywords

adaptive controlattitude and position controldual quaternionsrelative dynamicssix-DOF

Mathematics Subject Classification ID

Adaptive control/observation systems (93C40) Automated systems (robots, etc.) in control theory (93C85) Control of mechanical systems (70Q05)

Related Items (7)

A Super-Twisting Fault-Tolerant Control Based on Dual-Quaternion Formalism for Spacecraft Rendezvous ⋮ Finite-time and attitude tracking of a rigid body ⋮ Synthesis of control of spatial motion of a rigid body using dual quaternions ⋮ Spacecraft formation flying in the port-Hamiltonian framework ⋮ Twistor-based pose control for asteroid landing with path constraints ⋮ Quaternion methods and regular models of celestial mechanics and space flight mechanics: the use of Euler (Rodrigues-Hamilton) parameters to describe orbital (trajectory) motion. I: Review and analysis of methods and models and their applications ⋮ Solution of an inverse kinematics problem using dual quaternions

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