| 1. | Design of the power management module for micro - satellite 小卫星电源管理模块的设计 |
| 2. | A simple model of unregulated bus satellite power system is tested 本文针对卫星电源测试评估系统进行了软硬件系统的设计工作。 |
| 3. | Developing satellite power test and evaluate system is of great importance 因此,对卫星电源系统进行测试和评估具有十分重要的意义。 |
| 4. | Satellite power sub - system is one of the essential systems in satellite 卫星电源系统是星上产生、贮存、变换、调节和分配电能的系统。 |
| 5. | Based on the concept of virtual instrument , a satellite power test and evaluation system is developed 本文设计了一种基于太阳能电池阵模拟器和电子负载可编程功能的卫星电源测试评估系统。 |
| 6. | The structure and the relation of related component of the power system of satellite was analyzed in chapter 3 第三章分析了卫星电源系统的结构及相关元件的关系,对电源的测点及遥测值进行了研究。 |
| 7. | In the thesis , relative knowledge of satellite orbit and attitude is introduced . then the analyzing and designing for the hxmt solar panel & storage battery power system are given . the simulation algorithm and models are finally set up on it 本文首先介绍了与论文设计仿真相关的卫星轨道和卫星姿态动力学的概念和内容,对hxmt天文卫星电源系统? ?太阳能电池-蓄电池组电源系统的方案进行了分析和设计,建立了太阳能电池-蓄电池组电源系统仿真算法。 |
| 8. | The thesis is based on the subproject of national " 973 " key project , " hxmt spacecraft integral analysis and design " . aiming at the satellite power system , it establishes a simulation software , and uses it on the hxmt power system designing and simulation 本文以国家973专项课题“天体高能辐射的空间观测与研究”的子课题“ hxmt卫星系统方案设计”为应用背景,构造了一个面向卫星电源系统的仿真软件,并对hxmt天文卫星电源系统进行了设计分析和仿真工作。 |
| 9. | Solar array simulator is programmed in labview to simulate the running condition of satellite ( such as sun angle , shadow time , orbit and so on ) . electronic load is programmed in labview to simulate the running condition of satellite load . by data collecting and processing , satellite power engineers can monitor and evaluate working condition of satellite power system 该测试评估系统应用labview软件对太阳能电池阵列模拟器进行编程,模拟太阳能电池在空间各种状态下(轨道、光照角、进出阴影等)的情况;对电子负载进行编程,模拟卫星负载的各种变化(平均负载、短期负载和脉冲负载)情况,信号采集和数据处理单元在测试评估系统运行过程中记录电源系统各组成部分的工作参数,据此对卫星电源系统进行测试和评估。 |