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首页> 外文期刊>International journal of aerospace engineering >Gliding-Guided Projectile Attitude Tracking Controller Design Based on Improved Adaptive Twisting Sliding Mode Algorithm
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Gliding-Guided Projectile Attitude Tracking Controller Design Based on Improved Adaptive Twisting Sliding Mode Algorithm

机译:基于改进自适应扭转滑动模式算法的滑翔引导射弹姿态跟踪控制器设计

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摘要

The finite-time attitude tracking control for gliding-guided projectile with unmatched and matched disturbance is investigated. An adaptive variable observer is used to provide estimation for the unmeasured state which contains unmatched disturbance. Then, an improved adaptive twisting sliding mode algorithm is proposed to compensate for the matched disturbance dynamically with better transient quality. Finally, a proof of the finite-time convergence of the closed-loop system under the disturbance observer and the adaptive twisting sliding mode-based controller is derived using the Lyapunov technique. This attitude tracking control scheme does not require any information on the bounds of uncertainties. Simulation results demonstrate that the proposed method which is able to acquire the minimum possible values of the control gains guaranteeing the finite-time convergence performs well in chattering attenuation and tracking precision.
机译:研究了具有无与伦比和匹配干扰的滑动引导射弹的有限时间姿态跟踪控制。 自适应变量观察者用于提供包含无与伦比的干扰的未测量状态的估计。 然后,提出了一种改进的自适应扭转滑动模式算法以通过更好的瞬态质量来补偿匹配的干扰。 最后,使用Lyapunov技术导出了扰动观察者下闭环系统的有限时间收敛性的证据,并使用Lyapunov技术导出基于自适应扭转滑动模式的控制器。 这种态度跟踪控制方案不需要有关不确定性范围的任何信息。 仿真结果表明,该方法能够获取控制增益的最小可能值的方法,保证了有限时间收敛在抖动衰减和跟踪精度方面的表现良好。

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  • 来源
    《International journal of aerospace engineering 》 |2020年第4期| 1480427.1-1480427.15| 共15页
  • 作者

    Zhang Wenguang; Yi Wenjun;

  • 作者单位

    Nanjing Univ Sci & Technol Natl Key Lab Transient Phys Nanjing 210094 Peoples R China;

    Nanjing Univ Sci & Technol Natl Key Lab Transient Phys Nanjing 210094 Peoples R China;

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  • 正文语种 eng
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