Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Spacecraft integrated electronic system construction method and device

An integrated electronic system and integrated electronic technology, which is applied in the field of spacecraft integrated electronic system construction, can solve the problems that cannot meet the needs of the rapid development of the aerospace industry, does not solve the problem of customization, and is long.

Pending Publication Date: 2022-04-29
SHANGHAI AEROSPACE SYST ENG INST
View PDF0 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, due to the improvement of the functional integration of the integrated electronic system, the coupling with other subsystems of the whole device is relatively high, so its design iteration process is extremely complicated and long, and it often does not have advantages in the development cycle, and it affects the whole body. A requirement change may lead to repetition of the entire system development work
Therefore, only improving the functional integration without solving the customization problem cannot meet the requirements of rapid development and cannot meet the needs of the rapid development of my country's aerospace industry

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Spacecraft integrated electronic system construction method and device
  • Spacecraft integrated electronic system construction method and device
  • Spacecraft integrated electronic system construction method and device

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0028] The present invention will be described in detail below based on specific embodiments and with reference to the accompanying drawings. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0029] In order to solve the problems of decentralized development of large or multi-chamber spacecraft electronic systems in the prior art, difficulty in overall planning of resources, poor adaptability to demand changes, long development cycle, and high development costs, the invention provides a design of a modular distributed integrated electronic system for spacecraft Scheme, the specific implementation method is as follows.

[0030] figure 1 It is a flow chart of steps of a method for constructing an integrated electronic system of a spacecraft provided by an embodiment of the present invention.

[0031] Such as figure 1 As shown, the construction method of the spacecraft inte...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention discloses a method and a device for constructing a comprehensive electronic system of a spacecraft. The method comprises the following steps of: determining functional modules contained in the comprehensive electronic system of the spacecraft and the number of functions or interfaces corresponding to each functional module; constructing interface specifications among the functional modules; determining the number of comprehensive electronic units contained in the spacecraft and the function range of each comprehensive electronic unit; iterating the function range and the function module of each integrated electronic unit; and according to the current function and interface number demand, selecting target function modules to be combined into an integrated electronic unit of each partition, thereby forming the integrated electronic system of the spacecraft. According to the spacecraft integrated electronic system construction method disclosed by the invention, the constructed spacecraft integrated electronic system is high in function integration level, high in resource reuse degree, good in generalization degree and high in demand strain capacity.

Description

technical field [0001] The invention belongs to the technical field of aerospace integrated electronics, and in particular relates to a method and device for constructing an integrated electronic system of a spacecraft. Background technique [0002] The traditional electronic system design scheme of spacecraft platform generally adopts a clear-cut subsystem division method, and disperses the electronic system or equipment in such as power supply, digital control, measurement and control, attitude control, propulsion, thermal control, etc. according to the large functional classification. in multiple subsystems. Due to the low functional density, the weight, power consumption and volume of the whole device are large, and the launch cost is high. The sub-systems are independent, the products developed are various, the development cost is high, and the hardware resources are difficult to coordinate and utilize. Moreover, the generalization degree of the equipment is extremely...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/20G06F30/15G06Q10/10
CPCG06F30/20G06F30/15G06Q10/103
Inventor 韩潇盖建宁王立胜涂志均王迪谈寅陈建岳张玉花章斌
Owner SHANGHAI AEROSPACE SYST ENG INST
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products