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首页> 外文期刊>International journal of micro air vehicles >Passively Stable Flapping Flight From Hover to Fast Forward Through Shift in Wing Position
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Passively Stable Flapping Flight From Hover to Fast Forward Through Shift in Wing Position

机译:通过悬停位置的被动稳定拍打飞行,从悬停飞向快进

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摘要

Flapping Wing Micro Air Vehicles (FWMAVs) hold the potential to both cover large distances and perform precision flights when arrived at destination. However, flying at different speeds leads to a complex control problem for attitude stabilization. Inspired by nature, we present a morphing mechanism that allows tailed FW-MAVs to have a passively stabilized attitude both in fast forward flight and in slow hovering flight. The mechanism displaces the wings and hence aerodynamic center. It is implemented on the DelFly II and tested in-flight in a motion tracking arena. The experimental tests show that the morphing mechanism indeed allows to fly passively stable in multiple flight modes. Just changing the aerodynamic center allows the DelFly II to fly fast forward (similar to 6 m/s, pitch attitude of 10 degrees), transition to slow forward flight (similar to 0.8 m/s, pitch attitude of 55 degrees), and back. The proposed mechanism paves the way for FWMAVs performing long range missions such as search-and-rescue.
机译:扑翼式微型飞机(FWMAV)具有到达远距离并进行精确飞行的潜力。但是,以不同的速度飞行会导致姿态稳定的复杂控制问题。受自然界的启发,我们提出了一种变形机制,可使尾部FW-MAV在快进飞行和慢悬停飞行中均具有被动稳定的姿态。该机构使机翼移位,从而使空气动力学中心移位。它在DelFly II上实现,并在运动跟踪领域进行了飞行测试。实验测试表明,变形机制确实允许在多种飞行模式下被动稳定地飞行。只需更改空气动力学中心,DelFly II即可快速向前飞行(类似于6 m / s,俯仰姿态为10度),过渡到慢速向前飞行(类似于0.8 m / s,俯仰姿态为55度),然后向后飞行。拟议的机制为FWMAV进行远程任务(如搜索和救援)铺平了道路。

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