Wireless self-powered digital sun sensor

A solar sensor and self-powered technology, applied in the aerospace field, can solve the problems of increasing system power consumption and volume, high power consumption and low precision of digital solar sensors, and achieve improved measurement and calculation accuracy, miniaturization and autonomous modules High degree of modernization, flexible use and convenient effect

Active Publication Date: 2015-11-25
TSINGHUA UNIV
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AI Technical Summary

Problems solved by technology

[0004] In the related technology, the analog sun sensor is used, although its power consumption is low and it is easy to realize the self-power supply performance of the system, but due to the limitation of the analog photosensitive device, its accuracy is low and it is susceptible to interference
Compared with the sun sensor of the analog photosensitive device, the digital sun sensor based on CCD (Charge-coupled Device, electrically coupled device)/CMOS (Complementary Metal Oxide Semiconductor, Complementary Metal Oxide Semiconductor) device calculates the centroid position of the sun spot on the imaging surface Changes to achieve the calculation of the sun’s incident angle. Although its measurement accuracy is higher and its reliability is better, and it can accurately

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Embodiment Construction

[0031] A wireless self-powered digital solar sensor according to an embodiment of the present invention will be described below with reference to the accompanying drawings, and the same or similar reference numerals in the drawings represent the same or similar elements or elements with the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary only for explaining the present invention and should not be construed as limiting the present invention.

[0032] Embodiments of the present invention propose a wireless self-powered digital sun sensor.

[0033] figure 1 It is a structural block diagram of a wireless self-powered digital solar sensor according to an embodiment of the present invention.

[0034] like figure 1 As shown, the wireless self-powered digital solar sensor according to the embodiment of the present invention includes: a power module 100 , a MEMS light introducer 200 , a CMOS image detector 300 and an ele...

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Abstract

The invention provides a wireless self-powered digital sun sensor comprising a power module, an MEMS (micro electro mechanical system) light leading-in device, a CMOS (complementary metal oxide semiconductor) image detector and an electronic system, wherein the power module is used for supplying power to the wireless self-powered digital sun sensor; the MEMS light leading-in device comprises at least one group of asymmetrical hole patterns; the CMOS image detector is located below the MEMS light leading-in device and used for detecting light led by the MEMS light leading-in device and outputting row light intensity information of a sensing unit of the detector; the electronic system is used for managing energy supplied by the power module, calculating solar angles of two axes according to the row light intensity information and outputting the solar angles of two axes to an upper computer. The sun sensor is high in minimization and autonomous modularization degree, flexible and convenient to use, self-powered, capable of realizing wireless communication and capable of improving the measurement calculation accuracy of the solar angles of the two axes.

Description

technical field [0001] The invention relates to the field of aerospace technology, in particular to a wireless self-powered digital sun sensor. Background technique [0002] The sun sensor is an optical attitude sensor, which takes the sun as the observation object and is connected to the satellite platform. It can measure the sun's vector position according to the sun's incident light, and through the measurement of the sun's vector position, the sun sensor can provide Two-axis sun angle information, so that the orientation of the preset satellite in the body coordinate system can be determined, that is, the attitude of the satellite. [0003] In recent years, satellites have gradually developed towards miniaturization and miniaturization, which puts forward higher requirements for solar sensors, which require small size, light weight and low power consumption. [0004] In the related art, an analog sun sensor is used. Although it has low power consumption and is easy to r...

Claims

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Application Information

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IPC IPC(8): G01C1/00
CPCG01C1/00
Inventor 卫旻嵩邢飞尤政
Owner TSINGHUA UNIV
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