Control method for anti-short circuit of shunt regulation circuit in spacecraft power system

A technology of shunt regulation and power supply system, applied in battery circuit devices, circuit devices, current collectors, etc., can solve problems such as untimely, isolation, and complex judgment, and achieve stable and reliable operation, timely control response, and simple methods.

Active Publication Date: 2021-08-10
SHANGHAI INST OF SPACE POWER SOURCES
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AI Technical Summary

Problems solved by technology

This method has certain shortcomings: the judgment is complicated and not timely
After a short-circuit fault occurs in the regulating tube of the shunt regulation circuit, the ground needs to make a judgment based on the relevant telemetry data of the power system, and it is bound to be impossible to isolate the fault phenomenon in real time

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  • Control method for anti-short circuit of shunt regulation circuit in spacecraft power system
  • Control method for anti-short circuit of shunt regulation circuit in spacecraft power system
  • Control method for anti-short circuit of shunt regulation circuit in spacecraft power system

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Embodiment Construction

[0019] The following will combine Figure 1 to Figure 5 A further detailed description will be made on the control method for preventing short-circuit of the shunt regulation circuit of the spacecraft power supply system of the present invention.

[0020] Taking a spacecraft power supply system including 14 current shunt regulation circuits as an example, the short-circuit prevention control method of the spacecraft power supply system shunt regulation circuit of the present invention is described in detail.

[0021] figure 1 Shown is a functional block diagram of the control system of the shunt regulation circuit of the spacecraft power supply system in the preferred embodiment of the present invention.

[0022] The spacecraft power system shunt regulation circuit control system 37 includes:

[0023] 14-way shunt regulation circuit, respectively shunt regulation circuit 1, shunt regulation circuit 2, shunt regulation circuit 3, shunt regulation circuit 4, shunt regulation c...

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Abstract

In the anti-short circuit control method of the shunt adjustment circuit of the spacecraft power supply system of the present invention, the voltage reference row circuit adds a reference signal output on the basis of the original output n reference signals, and the voltage of the newly added reference signal is the smallest; for each shunt adjustment circuit , the working state of the regulating tube is controlled by the comparison result of the signal MEA and the original reference signal, and the working state of the protection tube is controlled by the comparison result of the signal MEA and the newly added reference signal; In the conduction state, the shunt adjustment function of each shunt adjustment circuit is realized by its own adjustment tube. According to the power demand of the load, the n-way shunt adjustment circuits supply power to the load in accordance with the sequential shunt adjustment control mode; when the adjustment tube of a certain shunt adjustment circuit In the event of a short-circuit fault, the shunt adjustment function of the shunt adjustment circuit is realized by its protection tube, and the shunt adjustment order of the shunt adjustment circuit is automatically adjusted to the last stage.

Description

technical field [0001] The invention relates to the field of space power supplies, in particular to a short-circuit prevention control method for a shunt regulation circuit of a spacecraft power supply system. Background technique [0002] At present, the spacecraft power system uses a solar array-battery power system. When the spacecraft is in the light period, it relies on the solar cell array to absorb solar energy to supply power to the load and charge the battery, and at the same time, the excess energy returns to the solar cell array through the short-circuit circuit of the shunt regulation circuit of the power supply system. In recent years, the requirements for the life, reliability and power output capability of the spacecraft power system have become higher and higher, and one of the key factors affecting the life and reliability of the spacecraft power system is the energy output and adjustment capabilities of the power system. With the increasing demand for spac...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H02J7/35
CPCH02J7/35
Inventor 程新韦云王胜佳薛鸿翔杨佩俞伟罗霄杨华
Owner SHANGHAI INST OF SPACE POWER SOURCES
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