基于智能算法的航天器温度监测与控制系统优化  

Optimization of spacecraft temperature monitoring and control system based on intelligent algorithm

作　　者：王学伟 王壮 WANG Xuewei;WANG Zhuang(Shandong Institute of Aerospace Electronics,Yantai 264000,China)

机构地区：[1]山东航天电子研究所,山东烟台264000

出　　处：《中国高新科技》2025年第3期19-21,共3页

摘　　要：文章利用智能算法对航天器温度监测与控制系统进行优化,提高其控制精度、响应速度及稳定性,保障航天器在多种复杂环境中正常工作。对航天器温度监测和控制系统理论基础进行阐述,包括温度监测原理、智能算法应用和系统优化理论框架等。对航天器温度监测与控制系统进行总体架构设计,对温度监测子系统及温度控制子系统设计方案进行详细规划。In this paper,intelligent algorithms are used to optimize the spacecraft temperature monitoring and control system,improve its control accuracy,response speed and stability,and ensure the normal operation of spacecraft in a variety of complex environments.The theoretical basis of the spacecraft temperature monitoring and control system is described,including the principle of temperature monitoring,the application of intelligent algorithm and the theoretical framework of system optimization.The overall architecture of spacecraft temperature monitoring and control system is designed,and the design scheme of temperature monitoring subsystem and temperature control subsystem is planned in detail.

关 键 词：航天器 温度监测与控制 智能算法 系统优化 

分 类 号：V448[航空宇航科学与技术—飞行器设计]