首页> 外文会议>Intelligent Engineering Systems, 1997. INES '97. Proceedings., 1997 IEEE International Conference on >A low-cost and low-weight attitude estimation system for an autonomous helicopter
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A low-cost and low-weight attitude estimation system for an autonomous helicopter

机译:用于自动直升机的低成本,轻型姿态估计系统

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In this paper a low-cost and low-weight attitude estimation system for an autonomous helicopter is presented. The system is based on an inclinometer and a rate gyro. The data coming from the sensors is fused through a complementary filter. In this way the slow dynamics of the inclinometer can be effectively compensated. Tests have shown that a very effective attitude estimation system can be achieved.
机译:本文提出了一种低成本,重量轻的自主直升机姿态估计系统。该系统基于测斜仪和速率陀螺仪。来自传感器的数据通过互补滤波器融合。这样,可以有效地补偿倾角仪的缓慢动态。测试表明,可以实现非常有效的姿态估计系统。

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