基于切换策略的翼伞轨迹跟踪控制
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1.南京航空航天大学;2.无人机研究院

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V249.1;TP273

基金项目:

173项目;JKW创新项目;国家重点研发计划重点专硕


Trajectory tracking control of parafoil based on switching strategy
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    摘要:

    针对翼伞系统轨迹跟踪控制中强扰动、大时滞性等问题,提出一种基于切换策略的翼伞轨迹跟踪控制器。结合线性自抗扰控制抗扰动能力强、响应速度快和预测控制能有效克服系统时滞性、跟踪精度高、鲁棒性好的优点,采用2维轨迹跟踪制导策略通过跟踪目标轨迹的航向角实现对翼伞轨迹的跟踪控制;在切换策略中,依据航向角偏差量设计了双切换量的控制器切换规则,降低了控制器间切换频率,提高了双控制器切换的可靠性。仿真结果表明,与单一的控制器相比,切换控制器对给定归航轨迹的跟踪具有更优的效果。

    Abstract:

    A trajectory tracking controller based on switching strategy is presented to solve the problem of strong disturbance and large time delay in parachute system trajectory tracking control. Combining the strong anti-disturbance ability, fast response speed and predictive control of linear auto-disturbance rejection control, the advantages of system delay, high tracking accuracy and good robustness can be overcome effectively. A 2-D trajectory tracking guidance strategy is used to track the parachute trajectory by tracking the heading angle of the target trajectory. In the switching strategy, a dual-switching controller switching rule is designed according to the heading angle deviation, which reduces the switching frequency between controllers and improves the reliability of the dual-controller switching. The simulation results show that the switching controller has better performance than a single controller in tracking a given homing trajectory.

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历史
  • 收稿日期:2022-11-28
  • 最后修改日期:2023-03-01
  • 录用日期:2023-02-02
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