基本信息:
- 专利标题: 소형 위성군을 위한 네비게이션 모듈 및 방법
- 专利标题(英):KR102233123B1 - Navigation module and method for small satellite constellation
- 申请号:KR1020190059755 申请日:2019-05-21
- 公开(公告)号:KR102233123B1 公开(公告)日:2021-03-29
- 发明人: 박재필 , 이성환 , 김도현 , 정인선 , 이광원 , 오형직
- 申请人: (주)나라스페이스테크놀로지
- 申请人地址: 서울특별시 서대문구...
- 专利权人: (주)나라스페이스테크놀로지
- 当前专利权人: (주)나라스페이스테크놀로지
- 当前专利权人地址: 서울특별시 서대문구...
- 代理人: 김재형
- 主分类号: G01S19/42
- IPC分类号: G01S19/42 ; G01S19/51 ; G01S19/25
A location providing device for a swarm flight according to an embodiment of the present invention is obtained by the second aircraft from a second aircraft performing the swarm flight together with a first aircraft including the location providing device at a first time point. A communication unit for receiving information on a GPS signal and information on a time interval at which the second vehicle acquires a GPS signal; A control unit determining a second time to store the GPS signal of the first vehicle based on the time interval; And a GPS receiver for receiving a GPS signal from a GPS satellite at the second time, wherein the control unit stores the GPS signal of the first flight vehicle at the second time, and the communication unit The aircraft receives information on the GPS signal acquired at the second time and information on the time interval, and the control unit is based on the time interval from a third time to the first aircraft at the second time. The relative position of the second aircraft may be calculated, and the calculated relative position may be numerically integrated to calculate the relative position of the second aircraft with respect to the first aircraft at the third time.
公开/授权文献:
- KR1020200134114A 소형 위성군을 위한 네비게이션 모듈 및 방법 公开/授权日:2020-12-01
信息查询:
EspacenetIPC结构图谱:
G | 物理 |
--G01 | 测量;测试 |
----G01S | 无线电定向;无线电导航;采用无线电波测距或测速;采用无线电波的反射或再辐射的定位或存在检测;采用其他波的类似装置 |
------G01S19/00 | 卫星无线电信标定位系统;利用这种系统传输的信号确定位置、速度或姿态 |
--------G01S19/01 | .传输时间戳信息的卫星无线电信标定位系统,例如,GPS |
----------G01S19/39 | ..传输带有时间戳信息的卫星无线电信标定位系统,例如GPS |
------------G01S19/42 | ...确定位置 |