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Dynamic tracking device and automatic guidance method based on 3D time-of-flight camera

机译:基于3d飞行时间相机的动态跟踪装置及自动导航方法

摘要

A beacon device uniquely identified by a Time-of-Flight camera. A dynamic tracking device [FIG. 1, (3)] includes a photoreceptor sensitive to light emission within a specific wavelength range, and a first optical signal [FIG. 1, (2c)]. A microcomputer [Fig. 1, Fig. 1, (2c)] that controls and controls the first light emitter [Fig. 1, (2c)] while contacting and calculating the light emitter and the three-dimensional information coming from the photo detector [Fig. 2a] and a second computer internal or external [FIG. 1 (2d)] incorporating data analysis, database services, media control and external mediation, and local or global data communication services. It has a three-dimensional camera [FIGS. 1 and 2] based on an of flight technology. In addition, the tracking device includes a beacon [FIG. 1, (1)] sensitive to an optical signal emitted from the first light emitter [FIG. 1 (2c)] of the three-dimensional camera [FIG. 1, (2)]. The beacon [FIG. 1, (1)] itself emits the second light of the optical signal [FIG. 2, (1b)] having a wavelength corresponding to the sensitivity of the three-dimensional camera [FIG. 1, (2)]. A beacon with a body. The beacon [FIG. 1, (1)] is an optical signal [FIG. 2, (1c, c ′, d)] emitted from the first light emitter of the optical signal [FIG. 1, (2c)]. Means for modulating. The three-dimensional camera is configured to measure a return time of a signal re-emitted by the beacon. The modulation is achieved by the beacon [FIG. 1, (1) in the three-dimensional volume covered by the field of view of the three-dimensional camera [FIG. 1, (2)] by the three-dimensional camera and at least two measured frames. ] Specific identification and simultaneous position determination are allowed. Unique identification of the beacon [FIG. 1, (1)] is achieved in the microcomputer by analysis of the apparent distance of the beacon in successive frames of the three-dimensional camera [FIG. 1, (2)]. [Selection] Figure 1
机译:飞行时间相机唯一标识的信标设备。动态跟踪设备[1,(3)]包括对特定波长范围内的光发射敏感的感光体,和第一光信号[图1,(3)]。 1,(2c)]。微型计算机[图[图1,图1,(2c)]控制和控制第一发光器[图1,图1,(2c)]。 [1,(2c)]接触并计算光发射器和来自光电探测器的三维信息[图1,(2c)]。 [2a]和第二台内部或外部计算机[图2a]。 1(2d)]合并了数据分析,数据库服务,媒体控制和外部中介以及本地或全局数据通信服务。它具有三维相机[图2D]。 [1和2]基于飞行技术。另外,跟踪设备包括信标[图2]。 [1,(1)]对从第一光发射器[图1]发射的光信号敏感。三维摄像机[图1(2c)]。 1,(2)]。信标[图。 [1,(1)]本身发射光信号的第二光[图2,(1)]。 [图2(1b)]具有与三维照相机的感光度相对应的波长。 1,(2)]。带有身体的信标。信标[图。 [图1,(1)]是光信号[图1。从光信号的第一光发射器发射的图2中的(1c,c',d)]是由光信号[1c,c',d)]形成的。 1,(2c)]。调节手段。三维摄像机被配置为测量由信标重新发射的信号的返回时间。调制是通过信标实现的。在图1中,(1)在三维体积所覆盖的三维摄像机的视野中[图1]。 [1,(2)]由三维摄像机和至少两个测量帧组成。允许特定的识别和同时的位置确定。信标的唯一标识通过分析三维摄像机连续帧中信标的视距,在微型计算机中实现[1,(1)]。 1,(2)]。 [选择]图1

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