首页> 中文期刊> 《计算机测量与控制》 >模块化航天器电源系统仿真研究

模块化航天器电源系统仿真研究

         

摘要

模块化航天器快速响应对迅速提高我国空间信息支援能力具有重大意义,所以为了快速增强我国空间实力,以快速响应为背景,对模块化航天器进行研究,首先介绍了模块化航天器及其快速集成测试方法,之后,以模块化航天器电源系统为例,通过数学模型搭建了其Simulink模型,主要对帆板面积,蓄电池容量,以及卫星在轨功率进行分析,最后,通过仿真结果验证了所建模型的准确性,为模块化航天器快速响应奠定了基础,同时提出了模块化航天器电源系统的快速响应应用模式.%The rapid response of modular spacecraft to rapidly improve the ability of space information support is of great significance,so in order to study the application of rapid response of modular spacecraft,this paper based on the rapid response studies the modular spacecraft,first introduces the modular spacecraft and the method of its rapid integration test,then taking the power system of modular spacecraft as an example,builds the Simulink model by mathematical model and mainly analyzes the area of panel,battery capacity,as well as satellite on-orbit power,finally,the accuracy of the model is verified by simulation,which lays the foundation for the rapid response of modular spacecraft and the paper presents a application model of rapid response of modular spacecraft power system.

著录项

相似文献

  • 中文文献
  • 外文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号