Microsatellite energy system

An energy system and micro-satellite technology, applied in the field of satellites, can solve problems such as complex circuit structure, converter circuit loss, and power consumption of the circuit, and achieve the effect of simplifying the circuit structure and ensuring maximum power output

Inactive Publication Date: 2017-01-25
48TH RES INST OF CHINA ELECTRONICS TECH GROUP CORP
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  • Summary
  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At the same time, the bus voltage setting value is inconsistent with the maximum power point voltage value of the solar cell array, so the DET method cannot maximize the use of solar cell power
[0005] (2) The circuit structure of the common MPPT energy transmission method is complex, and the voltage conversion and tracking algorithm implementation circuits all have power consumption
However, both the converter circuit and the maximum power point algorithm implementation circuit have power consumption
[0006] In addition, in some energy systems, when the charging current is too large, the method of directly cutting off the charging circuit is adopted, which not only brings energy loss, but also uses a relatively complicated MPPT method, and there are losses in the converter circuit and the maximum power point algorithm implementation circuit.

Method used

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Embodiment Construction

[0028] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.

[0029] Such as Figure 1 to Figure 5 As shown, the micro-satellite energy system of this embodiment includes a solar cell array 1, a charging management unit 2 with MPPT, a voltage conversion unit 3, a battery management unit 4 and an electric storage unit 5, and a charging management unit 2 with MPPT and a solar cell array 1 connected, used to set the output voltage of the solar cell array 1 to output the maximum power; the voltage conversion unit 3 is connected to the charging management unit 2 with MPPT, and used to convert the output voltage of the charging management unit 2 with MPPT into the required load Voltage; the battery management unit 4 is connected to the charging management unit 2 with MPPT and the storage unit 5 respectively, and is used to receive the output voltage of the charging management unit 2 with MPPT and output the sam...

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Abstract

The invention discloses a microsatellite energy system which comprises a solar array, a charging management unit with MPPT (maximum power point tracking), a voltage transformation unit, a battery management unit and an electric storage unit. The charging management unit with the MPPT is connected with the solar array and is used for setting output voltage of the solar array to output maximum power; the voltage transformation unit is connected with the charging management unit with the MPPT and is used for converting the output voltage of the charging management unit with the MPPT into voltage needed by loads; the battery management is connected with the charging management unit with the MPPT and the electric storage unit respectively and is used for receiving the output voltage of the charging management unit with the MPPT and outputting the output voltage identical to the electric storage unit. The microsatellite energy system has the advantages of being simple in structure, low in energy consumption, controllable in charging and discharging and the like.

Description

technical field [0001] The invention mainly relates to the field of satellite technology, in particular to a micro-satellite energy system. Background technique [0002] The satellite power system is one of the key subsystems of the satellite, which provides energy support for other subsystems and payloads of the satellite. The power system generally has two parts: "power supply system" and "power distribution system". The power supply system part is composed of power generation system and power control equipment, while the power generation system is composed of main power supply and energy storage battery. The main power supply is the satellite's primary power generator, converting other forms of energy into electricity. The energy storage power supply is the only energy source in the shadow area of ​​the satellite, and it also provides energy when the satellite has a peak power demand. The power control equipment completes the adjustment of the output power of the solar...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H02J7/35
CPCH02J7/35Y02E10/56
Inventor 张佳亮周蒙张建国杨晓生陆运章蒋超
Owner 48TH RES INST OF CHINA ELECTRONICS TECH GROUP CORP
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