具有固定倾斜旋翼和舵叶的垂直起降飞行器

IF 5.2 2区 计算机科学 Q2 ROBOTICS
Yongrae Kim, Sanghyuk Park
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引用次数: 0

摘要

本文描述了一种垂直起降(VTOL)飞机,该飞机配备了一个斜固定在机翼上的旋翼和一个改变螺旋桨滑流方向的控制面。传统的垂直起降飞机,如升力巡航或倾斜旋翼,要么会增加阻力和重量,导致效率和有效载荷能力降低,要么会增加机械复杂性,并伴随着复杂的控制要求。与其他传统的垂直起降飞机不同,这种飞行器仅仅通过改变飞机的俯仰姿态就能在固定翼和旋翼模式之间实现稳定的过渡。由于旋翼呈倾斜角度安装,不仅可以在悬停时控制俯仰,还可以在水平飞行时利用前后推力的差推力控制俯仰。此外,横摇角可以通过使用左右推力之间的差分推力来控制。此外,这架飞机通过改变旋翼滑流的方向来实现偏航轴控制。调节滑流方向的控制面被称为“舵叶”,它有望在悬停时提供快速的偏航响应,并在水平飞行时自然地增强方向稳定性。总体而言,这种设计有望提高能源效率,降低机械和软件复杂性,增强机动性,使车辆特别适合苛刻的现实操作环境。本文对一种带舵叶的定倾旋翼垂直起降飞机进行了数学建模,设计了飞机的控制律,并通过飞行试验进行了验证。
本文章由计算机程序翻译,如有差异,请以英文原文为准。

VTOL Air Vehicle With Fixed-Inclined Rotors and a Rudder Vane

VTOL Air Vehicle With Fixed-Inclined Rotors and a Rudder Vane

This paper describes a vertical take off and landing (VTOL) aircraft equipped with a rotor obliquely fixed to the wing and a control surface that changes the direction of the slipstream of the propeller. Conventional VTOL aircraft, such as lift-cruise or tilt rotor, show either increased drag and weight, resulting in reduced efficiency and payload capacity, or added mechanical complexity accompanied by sophisticated control requirements. Unlike other conventional VTOL aircraft, this vehicle achieves a stable transition between fixed-wing and rotary-wing modes simply by changing the pitch attitude of the aircraft. As the rotor is mounted at an inclined angle, it can control the pitch not only during hovering but also during horizontal flight by using differential thrust between the front and rear propulsion. Moreover, the roll angle can be controlled by using differential thrusts between the left and right thrusts. Additionally, this aircraft achieves yaw axis control by changing the direction of the rotor's slipstream. The control surface that adjusts the direction of the slipstream is termed the “rudder vane,” which is expected to provide rapid yaw response during hovering and naturally enhance directional stability during horizontal flight. Overall, this design promises improved energy efficiency, reduced mechanical and software complexity, and enhanced maneuverability, making the vehicle particularly well suited to demanding real-world operational environments. In this paper, mathematical modeling of a fixed-tilt rotor VTOL aircraft equipped with a rudder vane is performed, and a control law for the aircraft is designed and validated via flight tests.

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来源期刊
Journal of Field Robotics
Journal of Field Robotics 工程技术-机器人学
CiteScore
15.00
自引率
3.60%
发文量
80
审稿时长
6 months
期刊介绍: The Journal of Field Robotics seeks to promote scholarly publications dealing with the fundamentals of robotics in unstructured and dynamic environments. The Journal focuses on experimental robotics and encourages publication of work that has both theoretical and practical significance.
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