首页> 外文期刊>Aerospace science and technology >Error-constrained fixed-time trajectory tracking control for a stratospheric airship with disturbances
【24h】

Error-constrained fixed-time trajectory tracking control for a stratospheric airship with disturbances

机译:带有干扰的平流层飞艇的误区固定时间轨迹跟踪控制

获取原文
获取原文并翻译 | 示例
       

摘要

In this paper, a novel fixed-time trajectory tracking control method is presented for a six degrees of freedom (6-DOF) stratospheric airship with time-varying error constraints and disturbances. The tan-type barrier Lyapunov function (BLF) method is extended by the adding a power integrator technique to deal with the time-varying error constraints with the fixed-time stability guaranteed, which ensures that the convergence of a stratospheric airship to the reference trajectory can be achieved in a finite time regardless of its initial condition. Also the complex differential calculation is avoided in the backstepping design. A new fixed-time disturbance observer (DO), which counts on less prior knowledge of disturbances, is constructed to estimate the unknown disturbances. The proposed control method is developed based on the transformed error model, thus can be readily extended to a wide range of second-order mechanical systems. Finally, numerical simulations demonstrate the effectiveness of the proposed control scheme. (C) 2021 Elsevier Masson SAS. All rights reserved.
机译:在本文中,提出了一种新的固定时间轨迹跟踪控制方法,用于六个自由度(6-DOF)平流层飞艇,其时变误差约束和干扰。通过添加功率积分器技术来延长Tan型屏障Lyapunov函数(BLF)方法,以处理具有固定时稳定性的时变误差约束,确保了分流器飞艇到参考轨迹的收敛无论其初始条件如何,都可以在有限时间内实现。在BackStepping设计中也避免了复杂的差异计算。构建了一种新的固定时扰动观察者(DO),缺乏干扰的较少知识,以估计未知的干扰。所提出的控制方法是基于变换的误差模型开发的,因此可以容易地扩展到各种二阶机械系统。最后,数值模拟证明了所提出的控制方案的有效性。 (c)2021 Elsevier Masson SAS。版权所有。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号