2018
DOI: 10.1177/1687814018766741
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Passivity-based control for rocket launcher position servo system based on improved active disturbance rejection technology

Abstract: In order to achieve high motion accuracy and better robustness of the rocket launcher position servo system driven by a permanent magnet synchronous motor, a passivity-based controller based on improved active disturbance rejection control is proposed in this article. The convenient method of interconnection and damping assignment and passivitybased control is adopted to establish the port-controlled Hamiltonian system with dissipation model of permanent magnet synchronous motor. To further enhance the robustn… Show more

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Cited by 3 publications
(2 citation statements)
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“…The ESO estimates both the states of disturbances and feed-forward compensation. [20][21][22][23][24] ADRC cannot achieve a perfect performance and the controlled systems have poor response characteristics if reasonable ADRC parameters cannot be found. The optimal ADRC parameters can be used in robot joints to maximize the jumping and running abilities of robots.…”
Section: Introductionmentioning
confidence: 99%
“…The ESO estimates both the states of disturbances and feed-forward compensation. [20][21][22][23][24] ADRC cannot achieve a perfect performance and the controlled systems have poor response characteristics if reasonable ADRC parameters cannot be found. The optimal ADRC parameters can be used in robot joints to maximize the jumping and running abilities of robots.…”
Section: Introductionmentioning
confidence: 99%
“…A linear system was used to compensate for the actual system as the nominal system to solve the aircraft attitude tracking problem accurately and efficiently under uncertain model and external disturbances [12]. Wang Ronglin applies ADRC to a position servo system of a rocket launcher driven by a PMSM, which improves the movement accuracy and robustness of the servo system [13]. A nonaffine nonlinear system with unknown external perturbation was used to estimate the unknown parts of a system using ESO, thereby solving the difficult problem of virtual control derivative acquisition [14,15].…”
Section: Introductionmentioning
confidence: 99%