Li J, Ge J, Zhang G, Li Y, Wu L, Wu X, Fan S
Airborne Survey and Remote Sensing Center of Nuclear Industry, Shijiazhuang 050002, China.
School of Automation, China University of Geosciences, Lumo Road, Wuhan 430074, China.
Rev Sci Instrum. 2024 Jul 1;95(7). doi: 10.1063/5.0186906.
An unmanned helicopter is one of the main platforms for conducting unmanned aerial vehicle aeromagnetic measurements and combines the advantages of rotary-wing and fixed-wing unmanned aerial vehicles. However, unmanned helicopter-based aeromagnetic measurement systems face complex static magnetic noise and maneuvering magnetic interference, which limit their practical performance. To address this issue, an improved multi-channel frequency measurement algorithm for the optically pumped magnetic sensor is proposed to suppress the static magnetic noise proportional to the frequency noise generated by the random quantization error and the airborne electromagnetic interference. A novel aeromagnetic compensation method for the maneuvering magnetic interference is then proposed to weaken the negative effects of the strong multicollinearity of the attitude parameters of the unmanned helicopter on the compensation accuracy and stability by introducing a regularization term and weight matrix. In addition, dedicated software is developed for the real-time calculation and compensation of magnetic interference fields. A dedicated unmanned-helicopter-based aeromagnetic measurement system is developed, and ground and flight experiments are carried out. The ground test results indicate that the static noise of the proposed system is only 0.000 82 nT. In the flight experiments, the system achieves an improvement ratio of 8.33, which is higher than the improvement ratio of 4.37 for a state-of-the-art commercial compensator. Furthermore, the dynamic noise after compensation decreases by 37.6% from 0.0157 to 0.0098 nT.
无人直升机是进行无人机航磁测量的主要平台之一,它兼具旋翼无人机和固定翼无人机的优点。然而,基于无人直升机的航磁测量系统面临复杂的静磁噪声和机动磁干扰,这限制了它们的实际性能。为解决这一问题,提出了一种改进的光泵磁传感器多通道频率测量算法,以抑制与随机量化误差和机载电磁干扰产生的频率噪声成比例的静磁噪声。随后提出了一种针对机动磁干扰的新型航磁补偿方法,通过引入正则化项和权重矩阵,削弱无人直升机姿态参数强多重共线性对补偿精度和稳定性的负面影响。此外,开发了用于磁干扰场实时计算和补偿的专用软件。研制了一套基于无人直升机的专用航磁测量系统,并进行了地面和飞行试验。地面测试结果表明,所提系统的静态噪声仅为0.000 82 nT。在飞行试验中,该系统实现了8.33的改进率,高于一款先进商用补偿器4.37的改进率。此外,补偿后的动态噪声从0.0157 nT降至0.0098 nT,降低了37.6%。