一种纵列双旋翼跨介质无人机出入水切换控制
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TP273

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国家自然科学基金青年科学基金项目(62503486);国家自然科学基金面上项目(12572408);广东省重点领域研发计划项目(2025B1111130002);广东省特支计划项目(2023TX07A477);南方海洋科学与技术广东省实验室(珠海)项目(SML2024SP007).


A switching control method of tandem dual-rotor HAUVs for water entry and exit
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    摘要:

    为确保跨介质飞行过程的平稳性, 设计一种纵列式双旋翼跨介质无人机的切换控制方法. 该跨介质无人机在空中和水下采用两种不同的执行机构, 且空中存在欠驱动特性, 给跨介质无人机出入水的平稳控制带来了巨大挑战. 首先, 通过牛顿-欧拉方法, 给出一种新型纵列式双旋翼跨介质无人机在不同介质中的动力学模型; 然后, 考虑在不同飞行阶段执行机构的切换, 基于自适应超螺旋滑模方法, 提出一种新型的跨介质无人机姿态和高度的切换控制策略, 并设计合适的切换规则以确定控制器的切换时机; 接着, 利用李雅普诺夫稳定性理论, 验证闭环系统的渐近稳定性; 最后, 通过纵列式双旋翼跨介质无人机垂直出入水的仿真对所提出控制方法进行测试, 仿真结果验证了所设计控制器的有效性和鲁棒性.

    Abstract:

    In order to ensure the stability of trans-medium flight, a switching control method for a tandem dual-rotor hybrid aerial underwater vehicle (HAUV) is designed. This HAUV adopts two different sets of actuators in the air and underwater, and is underactuated during aerial flight, which brings huge challenges to the smooth control of the HAUV during water-entry and water-exit. Through the Newton-Euler method, the dynamic model of a new tandem dual-rotor HAUV across different media is established. Considering the switching of actuators in different flight stages, a new type of switching control strategy for the attitude and altitude of the HAUV is proposed based on the adaptive super-twisting sliding mode method, and a suitable switching rule is designed to determine the switching timing of controllers. The asymptotic stability of the closed loop system is proved using the Lyapunov stability theory. Finally, the proposed control method is tested via simulations of vertical water-entry and water-exit of the tandem dual-rotor HAUV, and the simulation results verify the effectiveness and robustness of the designed controller.

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张柏嘉,王继河,孙慧杰,等.一种纵列双旋翼跨介质无人机出入水切换控制[J].控制与决策,2026,41(6):1563-1576

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  • 收稿日期:2025-07-04
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  • 在线发布日期: 2026-05-13
  • 出版日期: 2026-06-10
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