An autonomous distribution control device on a launch vehicle rocket

A technology of power distribution control and launch vehicle, applied in the direction of circuit devices, electrical components, emergency power supply arrangements, etc., can solve the complex composition of ground power supply and distribution equipment, complex rocket-ground interfaces and rocket-ground cables, and do not conform to the intelligentization of electrical systems issues such as the development trend of the development trend, to achieve the effect of improving flexibility and maneuverability, strong flexibility and adaptability, and good task adaptability

Inactive Publication Date: 2018-12-21
SHANGHAI AEROSPACE SYST ENG INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] 1) The composition of ground power supply and distribution equipment is complex
[0005] Since the power supply and distribution control and sampling functions are all realized by ground equipment, the ground needs to be equipped with various control and sampling equipment such as control computer, measurement and control combination, transmission and control combination, and front-end and back-end PLC, resulting in a huge composition of ground power supply and distribution equipment. The interface relationship between ground equipment is complex, and there are a large number of control commands and test circuit interactions, which significantly increases the complexity of arrow-ground circuit design
[0006] 2) Low level of intelligence on the arrow
[0007] Since the distribution device on the arrow itself has no independent control and testing capabilities, it needs to use ground equipment and measurement systems to realize the power supply and distribution control and distribution parameter sampling of the electrical equipment on the arrow. The intelligent level of the arrow is low, which aggravates the work of the ground equipment Burden, not in line with the current development trend of electrical system intelligence;
[0008] As an important part of the electrical system of the launch vehicle, the power supply and distribution system of the launch vehicle is responsible for the power supply and distribution management and energy supply of the whole rocket's electrical equipment. The rocket and ground cables are complex. With the rapid development of electronic technology and integration technology, it is necessary to develop an autonomous power distribution control device on the launch vehicle with the characteristics of intelligence, autonomy and generalization, so as to realize the power supply and distribution of the rocket to the ground. Optimal configuration of equipment

Method used

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  • An autonomous distribution control device on a launch vehicle rocket

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Embodiment Construction

[0021] The autonomous power distribution control device on the launch vehicle of the present invention will be further described in detail in conjunction with the accompanying drawings and specific embodiments. Advantages and features of the present invention will be apparent from the following description and claims. It should be noted that all the drawings are in very simplified form and use imprecise ratios, which are only used for the purpose of conveniently and clearly assisting in describing the embodiments of the present invention.

[0022] Such as figure 1 As shown, an autonomous power distribution control device on a launch vehicle provided by the present invention includes a power supply module 10 , a communication control module 20 , a relay drive module 30 , a relay board module 40 , and a state monitoring module 50 .

[0023] The power supply module 10 is used for the self-power supply of the autonomous power distribution control device. The power supply is provi...

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Abstract

The invention relates to an autonomous distribution control device on a carrier rocket, which is composed of a power module, a communication control module, a relay driving module, a relay board module and a condition monitoring module. According to the test procedure, the power is supplied to the autonomous power distribution control device through the RS422 bus in turn, power-on and power-off commands, the communication control module outputs the corresponding IO control signal through the microprocessor after receiving the instruction, the signal power is amplified by the relay drive module, The corresponding relay in the relay board module is driven to operate so as to turn on or off the ground power supply or the path between the battery and the electric equipment. The condition monitoring module collects the distribution signals such as the internal voltage and current, and sends them to the external ground equipment for display and monitoring through the communication control module. As the RS422 bus communication is adopted between the rocket and the ground, and the autonomous distribution control device has a built-in microprocessor, the autonomous distribution control device on the carry rocket of the invention has the characteristics of good intelligence, autonomy and universality.

Description

technical field [0001] The invention relates to the field of power supply and distribution systems for launch vehicles, in particular to an autonomous power distribution control device on a launch vehicle. Background technique [0002] The launch vehicle is the foundation of space activities, and the electrical system is an important part of the launch vehicle. During ground testing and flight, it is necessary to supply and distribute power to the electrical equipment of the electrical system. The existing power supply and distribution equipment consists of equipment on the arrow and ground equipment. The equipment on the arrow includes batteries and distributors. Power distribution control between electrical equipment; ground equipment includes ground power supply, control microcomputer, measurement and control combination, transmission control combination and front-end PLC, etc., which are used to provide power supply, implement power distribution control and parameter sam...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H02J13/00H02J9/06
CPCH02J13/0062H02J9/061Y02B70/30Y02B90/20Y04S20/12Y04S20/248
Inventor 周恒保辛高波丁秀峰王猛但之华
Owner SHANGHAI AEROSPACE SYST ENG INST
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