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Stability and control of a quadrocopter despite the complete loss of one, two, or three propellers

机译:尽管一台,两台或三台螺旋桨完全丢失,但直升机的稳定性和控制能力

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This paper presents periodic solutions for a quadrocopter maintaining a height around a position in space despite having lost a single, two opposing, or three propellers. In each case the control strategy consists of the quadrocopter spinning about a primary axis, fixed with respect to the vehicle, and tilting this axis for translational control. A linear, timeinvariant description of deviations from the attitude equilibrium is derived, allowing for a convenient cascaded control design. The results for the cases of losing one and two propellers are validated in experiment, while the case of losing three propellers is validated in a nonlinear simulation. These results have application in multicopter fault-tolerant control design, and also point to possible design directions for novel flying vehicles.
机译:本文提出了一种直升机解决方案,该方案虽然失去了一个,两个相对的或三个螺旋桨,但仍能在空间位置保持高度附近的直升机。在每种情况下,控制策略都包括:直升机围绕主轴旋转(相对于车辆固定),并使该轴倾斜以进行平移控制。得出了与姿态平衡之间的偏差的线性时不变描述,从而可以方便地进行级联控制设计。在实验中验证了丢失一台和两台螺旋桨的情况的结果,而在非线性仿真中验证了丢失三台螺旋桨的情况的结果。这些结果已应用于多旋翼飞机的容错控制设计中,并指出了新型飞行器的可能设计方向。

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