Temperature control system and method for optimizing satellite energy use efficiency

A temperature control system and temperature controller technology, applied in the direction of temperature control using electric methods, can solve the problems of limited power stored in the battery, energy shortage, waste, etc., to reduce the possibility of heating, shorten the heating time, optimize Effect of heating sequence

Active Publication Date: 2018-10-19
AEROSPACE DONGFANGHONG SATELLITE
View PDF8 Cites 11 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Whether in the shaded area or in the sunny area, as long as the temperature of the control point is lower than the low temperature threshold, the temperature controller will start heating until the temperature reaches the high temperature threshold. Long-term heating increases the discharge depth of the battery, but it does not heat in the sunny area, and the power generation of the solar panel may be shunted and wasted in vain.
[0004] Especially for satellites with low orbits, the shadow time is relatively long, and in order to reduce atmospheric resistance, some satellites adopt the structure of body-mounted solar cells, such as gravity measurement satellites, due to the influence of the sun's illumination angle, the solar cell array will The power generation efficiency is low, the energy on the star is very tight, and the power stored in the battery is also very limited. If the battery energy is used too much in the shadow area for heating, the satellite may be in a dangerous state

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
  • Temperature control system and method for optimizing satellite energy use efficiency
  • Temperature control system and method for optimizing satellite energy use efficiency
  • Temperature control system and method for optimizing satellite energy use efficiency

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0026] Exemplary embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. Although exemplary embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure may be embodied in various forms and should not be limited by the embodiments set forth herein. Rather, these embodiments are provided for more thorough understanding of the present disclosure and to fully convey the scope of the present disclosure to those skilled in the art. It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other. The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0027] figure 1 A diagram of the temperature control system for optimizing energy use efficiency of the present invention. Such as figure 1 As shown, the t...

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 temperature control system and method for optimizing the satellite energy use efficiency. The system is composed of a power telemetering acquisition module, a power supply controller, a temperature controller, a heating loop, a temperature sensor and a remote control command unit. The power telemetering acquisition module collects state information. The remote control command unit is used for receiving remote control data sent by the ground and sending a first remote control command and a second remote control command. The power supply controller is used for calculating the residual energy of a satellite. The temperature sensor is used for collecting the temperature of a control point. The temperature controller controls connection or disconnection of the heatingloop according to the residual energy of a satellite, the temperature of the control point, a temperature control threshold parameter and a temperature control strategy. The heating loop is used for receiving controlling of the temperature controller and providing heat or stopping heat supply for a controlled temperature area. According to the invention, the power generating capacity of the solarcell array is used fully; the power wasting is reduced; the discharging electricity amount of the storage battery in a shadow area is reduced; and the energy utilization efficiency of the satellite isincreased effectively.

Description

technical field [0001] The invention belongs to the field of satellite intelligent temperature control, and in particular relates to a temperature control system and method for optimizing satellite energy use efficiency. Background technique [0002] In satellites at home and abroad, the temperature control method of high and low temperature thresholds is widely used, and there is generally a temperature range of several degrees or more than ten degrees between the high and low temperature thresholds. The on-board temperature controller collects the temperature value of the control point and compares it with the high and low temperature thresholds. When the temperature of the control point is lower than the low temperature threshold, it starts heating, and when it is higher than the high temperature threshold, it stops heating. When it is between the high and low temperature thresholds, it keeps At present, the heating state remains unchanged, so that the controlled equipmen...

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): G05D23/19
CPCG05D23/19
Inventor 伍保峰李松明仇越毕成史文龙
Owner AEROSPACE DONGFANGHONG SATELLITE
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products