发明名称 |
ANTENNA ATTITUDE MEASUREMENT SENSOR AND ANTENNA ATTITUDE MEASUREMENT METHOD |
摘要 |
The invention relates to an antenna attitude measurement sensor as well as an attitude measurement method based on this sensor, wherein the antenna attitude measurement sensor is composed of a solar position sensor, a three axial gravity acceleration sensor, a GPS module, a CPU, a power supply module and a memory output module. Antenna attitude measurement method includes the following steps: A. installing antenna attitude measurement sensor; B. acquiring antenna geographic location, antenna hanging height, antenna pitch angle γ and rolling angle θ as well as the incident sunlight azimuth angle φ related to the solar position sensor and the corresponding standard time to form the azimuth angle; C. calculating the vertical incident angle α and level incident angle β; D calculating the antenna azimuth δ; E. memory output. |
申请公布号 |
US2015260513(A1) |
申请公布日期 |
2015.09.17 |
申请号 |
US201314434627 |
申请日期 |
2013.09.30 |
申请人 |
Bi Shijie |
发明人 |
Bi Shijie |
分类号 |
G01B21/22;G01P15/00;G01C21/02;G01S19/00 |
主分类号 |
G01B21/22 |
代理机构 |
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代理人 |
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主权项 |
1. An antenna attitude measurement sensor including:
a solar position sensor, a three axial gravity acceleration sensor, a GPS module, a CPU, a power supply module and a memory output module, wherein: an input end of the CPU is respectively connected with the output ends of the solar position sensor, the three axial gravity acceleration sensor and the GPS module; an output end of CPU is connected with the memory output module; the power supply module is respectively connected with the solar position sensor, the three axial gravity acceleration sensor, GPS module, the central processor unit (CPU) and the memory output module. |
地址 |
Beijing CN |