• Electronics Optics & Control
  • Vol. 29, Issue 4, 89 (2022)
WANG Panwei, HOU Yuanlong, and WU Liang
Author Affiliations
  • [in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2022.04.017 Cite this Article
    WANG Panwei, HOU Yuanlong, WU Liang. ITAE-Based Design of Position Controller for Shipborne Rocket Launcher[J]. Electronics Optics & Control, 2022, 29(4): 89 Copy Citation Text show less

    Abstract

    ITAE optimal control enables the integral of time multiplied by absolute error to be the minimum in a system.ITAE has the characteristics of third-order no static errorthat isno error for uniform acceleration input.No-static-error ITAE optimal control method is simple and easy to implement in engineering.Howeveras for shipborne rocket launcher systems with time-varying parametersthe effect of directly using ITAE control is not idealbecause the parameters of the controller no longer meet the ITAE optimal transfer function due to the change of system parameters.Thereforeit is necessary to identify the system so that the parameters of the controller can change with the systems parameters.There are many methods for system identificationbut they do not meet the real-time requirements of shipborne rocket launcher.Thereforean easy-to-implement identification method is proposed in consideration of the performance requirements of weapon systems.The proposed algorithm is applied to ITAE parameter tuningand the results show that the proposed algorithm can effectively tune the parameters of ITAE controller of the servo system.
    WANG Panwei, HOU Yuanlong, WU Liang. ITAE-Based Design of Position Controller for Shipborne Rocket Launcher[J]. Electronics Optics & Control, 2022, 29(4): 89
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