2021
DOI: 10.34133/2021/9874563
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A High-Efficient Finite Difference Method for Flexible Manipulator with Boundary Feedback Control

Abstract: The paper presents a high-efficient finite difference method for solving the PDE model of the single-link flexible manipulator system with boundary feedback control. Firstly, an abstract state-space model of the manipulator is derived from the original PDE model and the associated boundary conditions of the manipulator by using the velocity and bending curvature of the flexible link as the state variables. Then, the second-order implicit Crank-Nicolson scheme is adopted to discretize the state-space equation, … Show more

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Cited by 14 publications
(6 citation statements)
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“…The obtained results would be applied to the automatic parking, automated warehouse system, and production assembly line. Further work entails investigating the region based tracking control of spacecraft [50,51] or flexible manipulator systems [52], and addressing broader performance aspects.…”
Section: Discussionmentioning
confidence: 99%
“…The obtained results would be applied to the automatic parking, automated warehouse system, and production assembly line. Further work entails investigating the region based tracking control of spacecraft [50,51] or flexible manipulator systems [52], and addressing broader performance aspects.…”
Section: Discussionmentioning
confidence: 99%
“…In addition, attacking a maneuvering target with multiple missiles is challenging due to the unknown interference in the guidance system caused by the unpredictable target's maneuverability. Furthermore, owing to the short flight time of terminal guidance, the guidance errors should be eliminated as fast as possible to meet the hitting accuracy requirement 18‐21 . Wang et al 22 proposed a robust cooperative guidance law with asymptotic convergence against a maneuvering target, which has an unsatisfactory convergence rate.…”
Section: Introductionmentioning
confidence: 99%
“…Furthermore, owing to the short flight time of terminal guidance, the guidance errors should be eliminated as fast as possible to meet the hitting accuracy requirement. [18][19][20][21] Wang et al 22 proposed a robust cooperative guidance law with asymptotic convergence against a maneuvering target, which has an unsatisfactory convergence rate. In order to obtain a faster convergence rate of the guidance errors, some studies have been conducted to design guidance laws based on the finite-time control theory.…”
Section: Introductionmentioning
confidence: 99%
“…The main challenges related to attitude maneuvering of large flexible spacecraft are related to the following aspects: (i) accurate modeling of the actuator dynamics, through inclusion of the gyroscopic terms, which affect the actual torque transferred to the spacecraft, (ii) accurate modeling of flexibility, and (iii) robustness with respect to parameter uncertainty, including the spacecraft mass distribution. Liu and Jin [7] describe a highly efficient finite difference method for modeling a single-link flexible manipulator. Tahmasebi and Esmailzadeh [8] present a quick approach for modeling and controlling a spacecraft equipped with three reaction wheels and two large flexible panels.…”
Section: Introductionmentioning
confidence: 99%