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Performance Test of a Hovering Flapping Wing Micro Air Vehicle with Double Wing Clap-and-Fling Mechanism

机译:双翼拍摄机构悬停悬停翼微型空气车的性能测试

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We present our hovering Flapping-Wing Micro Air Vehicle (FW-MAV) named Temasek Laboratories FlowerFly (TL-FlowerFly) having four wings and double clap-and-fling mechanism driven by only one motor. The TL-FlowerFly with a wing span of 22 cm from wing tip-to-wing tip and weight of 16.6 grams is fully integrated radio control system for manually control of motor speed and pitch-, yaw-, and roll-control. Double wing clap-and-fling is created by four wings at both end of downstroke and upstroke. In this work, gearbox has been modified from the original design to make its flapping angle more close to the sinusoidal function in order to reduced inertia effect. The TL-FlowerFly can perform flight like a helicopter: vertical take-off and landing, forward and backward flight, left and right flight, rotation around its body axis, and hovering. Powered by an onboard single cell LiPo battery (70 mAh, 3.7 V), it can endure five minutes of flight without payload, and 1.5 minutes with a 4 grams payload. Force measurement for various cases of wing slack angles indicated that 5° slack angle wing is the best for maximum thrust production. Moreover, power measurement was also conducted to characterize the flapping performance of the TL-FlowerFly. Free flight tests of the TL-FlowerFly was performed to verify the hovering stability and control effectiveness.
机译:我们展示了我们的悬停扑翼微型空气车(FW-MAV),名为Temasek Laboratories Flowerfly(TL-Flowerfly),只有四个电机驱动的四个翅膀和双拍摄机构。翼翼跨度距机翼尖端尖端和16.6克重量为22厘米的TL-Flowerfly是完全集成的无线电控制系统,用于手动控制电机速度和俯仰,偏航和滚动控制。双翼拍摄和漂浮在下游和上行程两端的四个翅膀上产生。在这项工作中,齿轮箱已经从原始设计中修改,以使其拍打角度更接近正弦函数,以减少惯性效应。 TL-Flowerfly可以像直升机一样进行飞行:垂直起飞和着陆,向前和向前飞行,左右飞行,围绕其体轴旋转,悬停。由板载单电池Lipo电池(70 MAH,3.7 V)提供动力,它可以忍受5分钟的航班,无需有效载荷,1.5分钟,4克有效载荷。各种机翼松弛角度的力测量表明,5°松弛角翼是最大的最大推力生产。此外,还进行了功率测量以表征TL-Flowerfly的拍打性能。进行TL-Flowerfly的免费飞行试验,以验证悬停稳定性和控制效果。

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