基于混合计算机接口的多旋翼飞行器3维空间目标搜索

Three-dimensional Space Target Search Based on Hybrid Computer Interfacefor Multi-rotor Aircraft

  • 摘要: 提出一种融合半自主导航、决策与接口转换子系统实现多旋翼飞行器室内3维空间目标搜索的混合计算机接口系统.半自主导航子系统为决策子系统提供2维空间可行飞行方向并实现多旋翼飞行器3维空间半自主避障.决策子系统采用联合回归模型与谱功率法从6个电极所采集的运动想象脑电信号中提取时域与频域特征,并利用支持向量机完成分类.接口转换子系统采用连续小波变换检测眨眼时的眼电特征,并通过分析这些眼动特征实现水平与垂直方向的运动想象任务接口切换.实际的室内3维空间目标搜索实验验证了该系统具有较好的适应性与控制稳定性;相比其他方法,半自主导航子系统降低了控制难度,控制精度约提高±10 cm.

     

    Abstract: A hybrid computer interface (HCI) system, composed of semi-autonomous navigation, decision and interface switching subsystems, is proposed to implement indoor 3-dimensional (3D) space target search for multi-rotor aircraft. The semi-autonomous navigation subsystem is utilized to provide 2-dimensional (2D) feasible directions for the decision subsystem and avoid obstacles semi-automatically in 3D space for multi-rotor aircraft. The decision subsystem applies the joint-regression (JR) model and spectral power methods to extracting the time and frequency domain features from motor imagery (MI) electroencephalogram (EEG) signals, which are collected by the 6 electrodes. Simultaneously, the support vector machine (SVM) is employed to complete the MI feature classification. The interface switching subsystem employs the continuous wavelet transform (CWT) method to identify electrooculography (EOG) features of eyeblink, and switch interfaces between horizontal and vertical MI tasks by analyzing the eyeblink EOG. The actual indoor 3D space target search experiment shows that the presented HCI system has good adaptability and control stability. Compared with similar methods, the semi-autonomous navigation subsystem reduces the control difficulties, and the control precision is increased by about ±10 cm.

     

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