公开(公告)号：US08976341B2

公开(公告)日：2015-03-10

申请号：US13967204

申请日：2013-08-14

Applicant: Korea Astronomy and Space Science Institute

Inventor： Seung Cheol Bang ,  Hyung Chul Lim ,  Jong Uk Park

IPC: G01S7/484 ,  G01S17/10 ,  G01S7/486

CPC classification number: G01S7/484 ,  G01S7/4865 ,  G01S17/105

Abstract: An optoelectric control apparatus for a satellite laser ranging system comprises a communication controller for externally receiving optoelectric control data. Memory is connected to the communication controller and stores a round trip distance to a satellite. A laser generation control unit is connected to the communication controller and outputs a laser fire signal. A signal measurement unit receives a laser start time. A real-time conversion unit is connected to the signal measurement unit and the communication controller, and converts a predicted laser arrival time into real time. A Lagrange interpolation processor is connected to the real-time conversion unit and the memory, and calculates a time at which laser light fired by a laser transmission unit returns back to a laser reception unit (laser arrival time). The clock unit is connected to a time measurement unit, the real-time conversion unit, a register unit, and a delay unit, and outputs time information.

Abstract translation: 一种用于卫星激光测距系统的光电控制装置，包括用于外部接收光电控制数据的通信控制器。 存储器连接到通信控制器并存储到卫星的往返距离。 激光产生控制单元连接到通信控制器并输出激光火焰信号。 信号测量单元接收激光开始时间。 实时转换单元连接到信号测量单元和通信控制器，并将预测的激光到达时间实时转换。 拉格朗日内插处理器连接到实时转换单元和存储器，并且计算由激光传输单元发射的激光返回激光接收单元（激光到达时间）的时间。 时钟单元连接到时间测量单元，实时转换单元，寄存器单元和延迟单元，并输出时间信息。

公开(公告)号：US20140118717A1

公开(公告)日：2014-05-01

申请号：US13967204

申请日：2013-08-14

Applicant: KOREA ASTRONOMY AND SPACE SCIENCE INSTITUTE

Inventor： Seung Cheol Bang ,  Hyung Chul Lim ,  Jong Uk Park

IPC: G01C3/08

CPC classification number: G01S7/484 ,  G01S7/4865 ,  G01S17/105

Abstract: An optoelectric control apparatus for a satellite laser ranging system comprises a communication controller for externally receiving optoelectric control data. Memory is connected to the communication controller and stores a round trip distance to a satellite. A laser generation control unit is connected to the communication controller and outputs a laser fire signal. A signal measurement unit receives a laser start time. A real-time conversion unit is connected to the signal measurement unit and the communication controller, and converts a predicted laser arrival time into real time. A Lagrange interpolation processor is connected to the real-time conversion unit and the memory, and calculates a time at which laser light fired by a laser transmission unit returns back to a laser reception unit (laser arrival time). The clock unit is connected to a time measurement unit, the real-time conversion unit, a register unit, and a delay unit, and outputs time information.

Abstract translation: 一种用于卫星激光测距系统的光电控制装置，包括用于外部接收光电控制数据的通信控制器。 存储器连接到通信控制器并存储到卫星的往返距离。 激光产生控制单元连接到通信控制器并输出激光火焰信号。 信号测量单元接收激光开始时间。 实时转换单元连接到信号测量单元和通信控制器，并将预测的激光到达时间实时转换。 拉格朗日内插处理器连接到实时转换单元和存储器，并且计算由激光传输单元发射的激光返回激光接收单元（激光到达时间）的时间。 时钟单元连接到时间测量单元，实时转换单元，寄存器单元和延迟单元，并输出时间信息。