TY - JOUR
T1 - Partial Lyapunov Strictification
T2 - Dual-Quaternion-Based Observer for 6-DOF Tracking Control
AU - Dong, Hongyang
AU - Hu, Qinglei
AU - Akella, Maruthi R.
AU - Mazenc, Frederic
N1 - Publisher Copyright:
© 1993-2012 IEEE.
PY - 2019/11
Y1 - 2019/11
N2 - Based on the dual-quaternion description, a smooth six-degree-of-freedom observer is proposed to estimate the incorporating linear (translational) and angular velocity, called the dual-angular velocity, for rigid bodies. To establish the observer, some important properties of dual vectors and dual quaternions are presented and proved, additionally, the kinematics of dual-transformation matrices is deduced, and the transition relationship between dual quaternions and dual transformation matrices is subsequently analyzed. An important feature of the observer is that all estimation states are ensured to be C∞ continuous, and estimation errors are shown to exhibit asymptotic convergence if the signals to be estimated are bounded. Furthermore, to achieve tracking control objectives, the proposed observer is combined with an independently designed proportional-derivative-like feedback control law (using full-state feedback), and a special Lyapunov 'strictification' process is employed to ensure a separation property between the observer and the controller, which further guarantees almost global asymptotic stability of the closed-loop tracking error dynamics. Numerical simulation results for a prototypical spacecraft pose tracking mission application are presented to illustrate the effectiveness and robustness of the proposed method.
AB - Based on the dual-quaternion description, a smooth six-degree-of-freedom observer is proposed to estimate the incorporating linear (translational) and angular velocity, called the dual-angular velocity, for rigid bodies. To establish the observer, some important properties of dual vectors and dual quaternions are presented and proved, additionally, the kinematics of dual-transformation matrices is deduced, and the transition relationship between dual quaternions and dual transformation matrices is subsequently analyzed. An important feature of the observer is that all estimation states are ensured to be C∞ continuous, and estimation errors are shown to exhibit asymptotic convergence if the signals to be estimated are bounded. Furthermore, to achieve tracking control objectives, the proposed observer is combined with an independently designed proportional-derivative-like feedback control law (using full-state feedback), and a special Lyapunov 'strictification' process is employed to ensure a separation property between the observer and the controller, which further guarantees almost global asymptotic stability of the closed-loop tracking error dynamics. Numerical simulation results for a prototypical spacecraft pose tracking mission application are presented to illustrate the effectiveness and robustness of the proposed method.
KW - Dual quaternion
KW - Lyapunov strictification
KW - pose tracking control
KW - six-degree-of-freedom (6-DOF) control
KW - velocity observer
UR - https://www.scopus.com/pages/publications/85052789546
U2 - 10.1109/TCST.2018.2864723
DO - 10.1109/TCST.2018.2864723
M3 - 文章
AN - SCOPUS:85052789546
SN - 1063-6536
VL - 27
SP - 2453
EP - 2469
JO - IEEE Transactions on Control Systems Technology
JF - IEEE Transactions on Control Systems Technology
IS - 6
M1 - 8454269
ER -