A robustness study of a finite‐time/exponential tracking continuous control scheme for constrained‐input mechanical systems: Analysis and experiments

2020 ◽  
Vol 30 (10) ◽  
pp. 3923-3944 ◽  
Author(s):  
Griselda I. Zamora‐Gómez ◽  
Arturo Zavala‐Río ◽  
Emilio Vázquez‐Ramírez ◽  
Fernando Reyes ◽  
Víctor Santibáñez
2018 ◽  
Vol 51 (22) ◽  
pp. 108-114 ◽  
Author(s):  
Griselda I. Zamora-Gómez ◽  
Arturo Zavala-Río ◽  
Daniela J. López-Araujo ◽  
Emmanuel Nuño ◽  
Emmanuel Cruz-Zavala

Author(s):  
Arturo Zavala‐Río ◽  
Griselda I. Zamora‐Gómez ◽  
Tonametl Sanchez ◽  
Fernando Reyes‐Cortes ◽  
Víctor Santibáñez

2013 ◽  
Vol 2013 ◽  
pp. 1-9 ◽  
Author(s):  
Wei Sun

This paper investigates the problem of finite-time tracking control for nonholonomic mechanical systems with affine constraints. The control scheme is provided by flexibly incorporating terminal sliding-mode control with the method of relay switching control and related adaptive technique. The proposed relay switching controller ensures that the output tracking error converges to zero in a finite time. As an application, a boat on a running river is given to show the effectiveness of the control scheme.


2020 ◽  
Vol 65 (2) ◽  
pp. 882-889 ◽  
Author(s):  
Griselda I. Zamora-Gomez ◽  
Arturo Zavala-Rio ◽  
Daniela J. Lopez-Araujo ◽  
Emmanuel Cruz-Zavala ◽  
Emmanuel Nuno

Author(s):  
Kejie Gong ◽  
Ying Liao ◽  
Yafei Mei

This article proposed an extended state observer (ESO)–based output feedback control scheme for rigid spacecraft pose tracking without velocity feedback, which accounts for inertial uncertainties, external disturbances, and control input constraints. In this research, the 6-DOF tracking error dynamics is described by the exponential coordinates on SE(3). A novel continuous finite-time ESO is proposed to estimate the velocity information and the compound disturbance, and the estimations are utilized in the control law design. The ESO ensures a finite-time uniform ultimately bounded stability of the observation states, which is proved utilizing the homogeneity method. A non-singular finite-time terminal sliding mode controller based on super-twisting technology is proposed, which would drive spacecraft tracking the desired states. The other two observer-based controllers are also proposed for comparison. The superiorities of the proposed control scheme are demonstrated by theory analyses and numerical simulations.


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