摘要
在分析羽流污染预示和太阳翼输出功率衰减预示方法基础上,识别出了影响羽流对太阳翼污染效应的关键因素,提出了较为系统的羽流对太阳翼污染效应的分析和控制方案。经仿真验证,该方法可有效实现量化分析和控制推力器羽流对太阳翼的污染效应,可以为我国卫星、深空探测和载人航天领域航天器工程研制提供参考。
In this paper,the plume contamination prediction and solar array power loss are analyzed,and the variables which are key factors to plume contamination effect are identified.And then,a systematic method for plume contamination effect analysis and control is proposed,which has been proved to be effective and measurable in simulations.The method and process proposed in this paper are also suggested as a reference for earth satellite,space exploration and manned spacecraft design.
出处
《航天器工程》
北大核心
2015年第4期58-64,共7页
Spacecraft Engineering
基金
国家重大科技专项工程