Anwar Ali, L. Reyneri, J. C. de los Rios, H. Ali, M. R. Mughal
{"title":"Reconfigurable magnetorquer for the CubePMT module of CubeSat satellites","authors":"Anwar Ali, L. Reyneri, J. C. de los Rios, H. Ali, M. R. Mughal","doi":"10.1109/INMIC.2012.6511478","DOIUrl":null,"url":null,"abstract":"This paper describes reconfigurable magnetorquer coil designed and implemented for the CubePMT (CubeSat power management tile) module of CubeSat. CubeSat has different modules and Power Management Tile (PMT) is the fundamental one. We designed Power Management Tile for the CubeSats, called CubePMT. It comprises of power supply, housekeeping and attitude sensors, on-board processor and attitude actuator. CubeSat requires precise and efficient attitude actuators subsystem. Magnetorquer coil is the most essential element of the attitude actuator subsystem. It generates magnetic field which interacts with the earth magnetic field and provides torque to the satellite. The goal of this work is to provide CubeSat with a magnetorquer coil which has small dimensions, less weight and low heat generation inside PCB. It should be reconfigurable and occupy no extra space on the spacecraft. It is integrated inside PCB four internal layers. Magnetorquer coil in each layer is treated as individual coil and is attached through switches. Changing the arrangements of these switches, one can use either a single coil, two, three or four coils in series or in parallel. This reconfigurable design gives a freedom in generating any amount of dipole moment and control power dissipation and heat generation inside the CubePMT module.","PeriodicalId":396084,"journal":{"name":"2012 15th International Multitopic Conference (INMIC)","volume":"28 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2012-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"6","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2012 15th International Multitopic Conference (INMIC)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/INMIC.2012.6511478","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 6
Abstract
This paper describes reconfigurable magnetorquer coil designed and implemented for the CubePMT (CubeSat power management tile) module of CubeSat. CubeSat has different modules and Power Management Tile (PMT) is the fundamental one. We designed Power Management Tile for the CubeSats, called CubePMT. It comprises of power supply, housekeeping and attitude sensors, on-board processor and attitude actuator. CubeSat requires precise and efficient attitude actuators subsystem. Magnetorquer coil is the most essential element of the attitude actuator subsystem. It generates magnetic field which interacts with the earth magnetic field and provides torque to the satellite. The goal of this work is to provide CubeSat with a magnetorquer coil which has small dimensions, less weight and low heat generation inside PCB. It should be reconfigurable and occupy no extra space on the spacecraft. It is integrated inside PCB four internal layers. Magnetorquer coil in each layer is treated as individual coil and is attached through switches. Changing the arrangements of these switches, one can use either a single coil, two, three or four coils in series or in parallel. This reconfigurable design gives a freedom in generating any amount of dipole moment and control power dissipation and heat generation inside the CubePMT module.
本文介绍了为CubeSat电源管理模块CubePMT (CubeSat power management tile)设计并实现的可重构磁振子线圈。CubeSat有不同的模块,电源管理模块(PMT)是最基本的模块。我们为立方体卫星设计了电源管理模块,称为CubePMT。它由电源、管家和姿态传感器、机载处理器和姿态执行器组成。立方体卫星需要精确、高效的姿态致动子系统。磁力矩线圈是姿态作动器子系统中最核心的元件。它产生磁场,与地球磁场相互作用,并为卫星提供扭矩。这项工作的目标是为CubeSat提供一个尺寸小,重量轻,PCB内部发热量低的磁振子线圈。它应该是可重新配置的,并且不占用航天器上的额外空间。它集成在PCB内部四层。每一层的磁致力矩线圈被视为单独的线圈,并通过开关连接。改变这些开关的安排,人们可以使用单线圈,两个,三个或四个线圈串联或并联。这种可重构设计可以自由地产生任意数量的偶极矩,并控制CubePMT模块内的功耗和热量产生。