首页> 外文会议>International astronautical congress >LOW COST, SYSTEMATIC SOFTWARE AND HARDWARE PROCESSES INCLUDING ON BOARD COMPUTER IN LOOP SIMULATION AND HARDWARE IN LOOP SIMULATIONS FOR 'PRATHAM' STUDENT SATELLITE, IIT BOMBAY
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LOW COST, SYSTEMATIC SOFTWARE AND HARDWARE PROCESSES INCLUDING ON BOARD COMPUTER IN LOOP SIMULATION AND HARDWARE IN LOOP SIMULATIONS FOR 'PRATHAM' STUDENT SATELLITE, IIT BOMBAY

机译:低成本,系统化软件和硬件过程,包括板载计算机,用于循环模拟,以及用于“ PRATHAM”学生卫星,IIT BOMBA的循环模拟中的硬件

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Students from the Indian Institute of Technology Bombay (IITB) are currently in the process of building a plug and play micro-satellite bus "Pratham" in collaboration with the Indian Space Research Organization. There are two main electronic boards on Pratham viz. On Board Computing board which hosts the core controller of the satellite, and the Power Board which distributes power to different loads on the satellite. The requirement imposed by ISRO on the success rate of electronic circuit boards in student satellite is 99%. The testing procedures are categorized as hardware testing and software testing. The paper will discuss the standard procedures followed mainly in Hardware testing of the aforementioned Electronic Circuit Boards involved in the making of Pratham. Step by step process for the hardware testing is used. The software testing is done by real time 'On-board In Loop Simulation (OILS)' where atmospheric and gravity conditions are simulated using standard environment models while GPS, magnetometer and magnetorquer are simulated by hardware interfaces that are mimicked exactly. This will test and validate the hardware interfaces and software accuracy. Sensors and actuators are simulated using Hardware In Loop Simulation (HILS). There are various sensors viz. GPS, Magnetometer and Sun-sensor which give input to the OBC board which then calculates the control inputs required to achieve the desired attitude. The setup used in testing these sensors/ actuators along with OBC board and their results are also included. The testing procedures in both the circuit boards are broken down into various levels with level 0 as fabrication and soldering precautions set by ISRO while final level as integrated testing of entire circuit board. A generalized and systematic troubleshooting procedure for Electronic Circuit Boards is included as well.
机译:印度孟买理工学院(IITB)的学生目前正在与印度航天研究组织合作,制造即插即用的微型卫星总线“ Pratham”。在Pratham viz上有两个主要的电子板。机载计算板,托管卫星的核心控制器,电源板,将功率分配给卫星上的不同负载。 ISRO对学生卫星中电子电路板成功率的要求为99%。测试过程分为硬件测试和软件测试。本文将讨论在制造Pratham涉及的上述电子电路板的硬件测试中主要遵循的标准程序。使用用于硬件测试的逐步过程。软件测试是通过实时的“车载回路内仿真(OILS)”完成的,其中使用标准环境模型来模拟大气和重力条件,而GPS,磁力仪和磁矩仪则是通过精确模拟的硬件接口来仿真的。这将测试并验证硬件接口和软件准确性。传感器和执行器使用硬件在环仿真(HILS)进行仿真。有各种传感器,即。 GPS,磁力计和太阳传感器向OBC板提供输入,然后OBC板计算出实现所需姿态所需的控制输入。还包括用于测试这些传感器/执行器以及OBC板的设置及其结果。两块电路板的测试程序分为多个级别,其中ISRO设置了0级作为制造和焊接预防措施,而最终级别则作为整个电路板的集成测试。还包括针对电子电路板的通用且系统的故障排除程序。

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