{"title":"研制LAPAN-A4卫星相机热功率识别数据记录仪软件","authors":"Gafur H.Z. Bahari, A. Syafrudin","doi":"10.1109/ICARES.2019.8914337","DOIUrl":null,"url":null,"abstract":"The process of testing and verification of satellite components is important to ensure that each sub-system can complete the task that has been designed. Thermal monitoring is important for the camera, therefore thermal measurement has to be accurate because changes in temperature can cause data error. Besides thermal, power requirements are one of the most important parameters in satellite development. This paper aims to conduct thermal and power testing from a data logger. The data logger which is an instrument to read data from time to time. From the test data, it can be seen that the ADC, PCB and Charge Coupled Device temperature at each Image Interface Modules will increase drastically when the camera is on the operation mode. The temperature at each Image Interface Modules increases for about 11.41° C, 13.61° C, 8.21° C and 7.81° C for ADC, PCB, Charge-Coupled Device channel 0 and Charge Coupled Device channel 1 respectively. Barrel temperature does not change significantly when the camera is turned on. Barrel temperature at each Image Interface Modules changes in the range 23C − 24C according to ambient temperature. For power consumption based on line period testing with line period mode using an altitude range of 485 km − 700 km. The initial power needed at an altitude of 485 km is 18.77 W. The power required at the simulation of 700 km altitude is 16.17 W.","PeriodicalId":376964,"journal":{"name":"2019 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology (ICARES)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2019-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"Development Data Logger Software For Thermal and Power Identification Of LAPAN-A4 Satellite Camera\",\"authors\":\"Gafur H.Z. Bahari, A. Syafrudin\",\"doi\":\"10.1109/ICARES.2019.8914337\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The process of testing and verification of satellite components is important to ensure that each sub-system can complete the task that has been designed. Thermal monitoring is important for the camera, therefore thermal measurement has to be accurate because changes in temperature can cause data error. Besides thermal, power requirements are one of the most important parameters in satellite development. This paper aims to conduct thermal and power testing from a data logger. The data logger which is an instrument to read data from time to time. From the test data, it can be seen that the ADC, PCB and Charge Coupled Device temperature at each Image Interface Modules will increase drastically when the camera is on the operation mode. The temperature at each Image Interface Modules increases for about 11.41° C, 13.61° C, 8.21° C and 7.81° C for ADC, PCB, Charge-Coupled Device channel 0 and Charge Coupled Device channel 1 respectively. Barrel temperature does not change significantly when the camera is turned on. Barrel temperature at each Image Interface Modules changes in the range 23C − 24C according to ambient temperature. For power consumption based on line period testing with line period mode using an altitude range of 485 km − 700 km. The initial power needed at an altitude of 485 km is 18.77 W. The power required at the simulation of 700 km altitude is 16.17 W.\",\"PeriodicalId\":376964,\"journal\":{\"name\":\"2019 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology (ICARES)\",\"volume\":\"1 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2019-10-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2019 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology (ICARES)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICARES.2019.8914337\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2019 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology (ICARES)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICARES.2019.8914337","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 1
摘要
卫星部件的测试和验证过程对于确保每个子系统能够完成已设计的任务非常重要。热监测对相机很重要,因此热测量必须准确,因为温度的变化会导致数据误差。除了热能之外,功率需求也是卫星研制中最重要的参数之一。本文的目的是通过数据记录仪进行热和功率测试。数据记录器是一种不时读取数据的仪器。从测试数据可以看出,当相机处于工作模式时,每个图像接口模块上的ADC、PCB和电荷耦合器件温度都会急剧升高。对于ADC、PCB、电荷耦合器件通道0和电荷耦合器件通道1,每个图像接口模块的温度分别升高约11.41°C、13.61°C、8.21°C和7.81°C。相机开机时,机筒温度变化不大。每个图像接口模块的桶温根据环境温度在23℃~ 24℃范围内变化。用于基于线周期测试的功耗,采用线周期模式,海拔范围为485 km ~ 700 km。在海拔485公里处所需的初始功率为18.77瓦。模拟海拔700公里时所需功率为16.17 W。
Development Data Logger Software For Thermal and Power Identification Of LAPAN-A4 Satellite Camera
The process of testing and verification of satellite components is important to ensure that each sub-system can complete the task that has been designed. Thermal monitoring is important for the camera, therefore thermal measurement has to be accurate because changes in temperature can cause data error. Besides thermal, power requirements are one of the most important parameters in satellite development. This paper aims to conduct thermal and power testing from a data logger. The data logger which is an instrument to read data from time to time. From the test data, it can be seen that the ADC, PCB and Charge Coupled Device temperature at each Image Interface Modules will increase drastically when the camera is on the operation mode. The temperature at each Image Interface Modules increases for about 11.41° C, 13.61° C, 8.21° C and 7.81° C for ADC, PCB, Charge-Coupled Device channel 0 and Charge Coupled Device channel 1 respectively. Barrel temperature does not change significantly when the camera is turned on. Barrel temperature at each Image Interface Modules changes in the range 23C − 24C according to ambient temperature. For power consumption based on line period testing with line period mode using an altitude range of 485 km − 700 km. The initial power needed at an altitude of 485 km is 18.77 W. The power required at the simulation of 700 km altitude is 16.17 W.