arXiv:2512.01246cs.RO2025-12中稿 · IEEE RA-L

双旋翼桨盘机构提升飞行效率与机动性,实现长续航自主飞行。

COMET: A Dual Swashplate Autonomous Coaxial Bi-copter AAV with High-Maneuverability and Long-Endurance

  • 采用双桨盘结构,优化旋翼系统效率与紧凑设计。
  • 飞行测试显示其比单桨盘方案更高效、轨迹跟踪更精准。
  • 适合对续航与灵活飞行有要求的无人机应用。

共轴双旋翼自主飞行器(AAV)因其潜在的旋翼系统高效率和紧凑外形而受到关注。然而,如何在共轴双旋翼系统中平衡效率、机动性和紧凑性仍是关键设计挑战,限制了其实际部署。本文介绍COMET,一种配备双桨盘机构的共轴双旋翼AAV平台。通过台架测试优化了旋翼系统的效率与紧凑性,并通过飞行续航实验验证了整机在不同载荷条件下的效率与鲁棒性。系统的机动性性能通过全面的轨迹跟踪测试进行评估。结果表明,双桨盘配置相比单桨盘方案显著提升了跟踪性能并改善了飞行效率。多种场景下的自主飞行试验成功验证了COMET在真实应用中的潜力。

原文摘要 · Abstract (English)

Coaxial bi-copter autonomous aerial vehicles (AAVs) have garnered attention due to their potential for improved rotor system efficiency and compact form factor. However, balancing efficiency, maneuverability, and compactness in coaxial bi-copter systems remains a key design challenge, limiting their practical deployment. This letter introduces COMET, a coaxial bi-copter AAV platform featuring a dual swashplate mechanism. The coaxial bi-copter system's efficiency and compactness are optimized through bench tests, and the whole prototype's efficiency and robustness under varying payload conditions are verified through flight endurance experiments. The maneuverability performance of the system is evaluated in comprehensive trajectory tracking tests. The results indicate that the dual swashplate configuration enhances tracking performance and improves flight efficiency compared to the single swashplate alternative. Successful autonomous flight trials across various scenarios verify COMET's potential for real-world applications.

无人机飞行控制双桨盘长续航

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