多通道双荷载六旋翼无人机动力输出优化控制
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TP273

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国家自然科学基金资助项目(52275051);重庆市教育委员会科学技术研究重点项目(KJZD-K202000701);重庆市技术创新与应用发展专项重点项目(cstc2019jscx-fxydX0028)


Design of high-performance six rotor unmanned aerial vehicle power system
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    摘要:

    六旋翼无人机动力系统受到电池功能以及应用环境动态变化等因素的影响,导致动力输出的稳定性不好,为了克服这一问题,提出基于多通道双荷载动态输出调整的六旋翼无人机动力系统设计和控制方法。首先分析六旋翼无人机动力输入参数,以无人机电机电磁转矩、电机转速参数、输出功率损耗和效率等为优化变量,采用多线程动态相匹配和兼容性调制方法,建立无人机动力输出的多通道双荷载动力匹配和任务调度模型,并根据无人机组的任务覆盖半径实现动力的自适应寻优控制,降低额外输出开销,提高无人机生存时间周期。测试结果表明,设计的无人机动力系统提高了搭载能力,能耗开销较小,动力输出的均衡性较好,提高了无人机的动力输出稳定性和飞行寿命。

    Abstract:

    The power system of six-rotor UAV is affected by the battery function and the dynamic change of application environment, which leads to the poor stability of power output. In order to improve the stability of power output of UAV, a design and control method of power system of six-rotor UAV based on multi-channel dual-load dynamic output adjustment is proposed. The power input parameters of six-rotor UAV are analyzed. Taking the electromagnetic torque of UAV motor, battery material cost, output power loss and efficiency as optimization variables, a multi-channel dual-load power matching and task scheduling model of UAV power output is established by using multi-thread dynamic matching and compatibility modulation methods. The adaptive optimization control of power is realized according to the task coverage radius of UAV, which reduces the extra output overhead and improves the life cycle of UAV. The test results show that the designed UAV power system has improved the carrying capacity, less energy consumption and better balance of power output, and improved the stability of power output and flight life of UAV.

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陈雅菲,邓涛. 多通道双荷载六旋翼无人机动力输出优化控制[J]. 科学技术与工程, 2024, 24(20): 8776-8782.
Chen Yafei, Deng Tao. Design of high-performance six rotor unmanned aerial vehicle power system[J]. Science Technology and Engineering,2024,24(20):8776-8782.

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历史
  • 收稿日期:2023-07-13
  • 最后修改日期:2024-04-30
  • 录用日期:2023-11-14
  • 在线发布日期: 2024-07-26
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