首页> 外文会议>58th International Astronautical Congress 2007 >RYERSON UNIVERSITY INITIATIVES IN DESIGN AND DEVELOPMENT OF MINIATURE SATELLITES INCLUDING FEMTO-SATELLITES
【24h】

RYERSON UNIVERSITY INITIATIVES IN DESIGN AND DEVELOPMENT OF MINIATURE SATELLITES INCLUDING FEMTO-SATELLITES

机译:RYERSON大学在设计和开发微型卫星(包括微型卫星)方面的举措

获取原文

摘要

Recently, Ryerson University has started work on design and development of miniature satellites under the author's supervision. These miniature satellites include 350 gm Can-sized satellite (RyCanSat), 1 kg pico-sized satellite (RyPicosat), and 100 gm femto-sized satellite (RyFemsat). The design of RyCanSat has been completed and it has undergone flight testing using a balloon and a rocket to an altitude of 3000 feet. This satellite won the first prize in the CanSat competition 2006 organised by American Astronatucal Society (AAS), American Institute of Aeronautics and Astronautics (AIAA), National Space Grant Consortia (NSGC), and Universities Space Research Association (USRA). ' RyPicosat and RyFemsat are in developmental stage. The primary objectives of RyPicosat mission are: (a) test and demonstration of onboard sensors (GPS receiver, sun sensor, rate sensor, magnetometer, onboard camera, temperature sensor), (b) test and demonstration of the flight computer used for RyCanSat, (c) flight qualification and certifications of various vendors' subsystems including MEMS based sensors (MEMS based rate sensor, sun sensor, temperature sensor, and others), (d) test design methodology for the development of cost-effective modular Picosatellites, and (e) test passive attitude stabilization using permanent magnet. RyFemsat is designed to be no bigger than a typical cell phone and it carries its own battery and charging circuit. This satellite is proposed for Ryerson femto formation flying experiment (RyF~3ex) missions: RyF3ex-l mission consists of two tethered femtosatellites while RyF3ex-2 mission involves a formation of multiple femto-satellites. The first mission will carry simple attitude sensors as payload and will serve to prove the viability of the data link to the ground. The main mission objectives are: (a) test command and control architecture and hardware, (b) formation keeping and reconfiguration control algorithms, (c) communications protocol and data relay, and (d) imaging of the Earth's surface. The paper presents in detail about the design and development of miniature satellites including formation flying mission.
机译:最近,瑞尔森大学开始在作者的指导下进行微型卫星的设计和开发。这些微型卫星包括350克Can大小的卫星(RyCanSat),1千克微微大小的卫星(RyPicosat)和100克毫微微大小的卫星(RyFemsat)。 RyCanSat的设计已经完成,并且已经使用气球和火箭对3000英尺的高度进行了飞行测试。该卫星在2006年由美国宇航学会(AAS),美国航空航天学会(AIAA),国家航天局财团(NSGC)和大学空间研究协会(USRA)举办的CanSat竞赛中获得了第一名。 RyPicosat和RyFemsat处于开发阶段。 RyPicosat任务的主要目标是:(a)测试和演示机载传感器(GPS接收器,太阳传感器,速率传感器,磁力计,机载相机,温度传感器),(b)测试和演示用于RyCanSat的飞行计算机, (c)各种供应商子系统的飞行资格和认证,包括基于MEMS的传感器(基于MEMS的速率传感器,太阳传感器,温度传感器等),(d)用于开发经济高效的模块化Picosatellite的测试设计方法,以及( e)使用永磁体测试被动姿态稳定性。 RyFemsat的设计尺寸不超过典型的手机,它带有自己的电池和充电电路。该卫星被建议用于Ryerson毫微微编队飞行实验(RyF〜3ex)任务:RyF3ex-1任务由两个系留的飞卫星组成,而Ry​​F3ex-2任务涉及多个毫微微卫星的编队。第一项任务将携带简单的姿态传感器作为有效载荷,并用于证明数据链接到地面的可行性。主要任务目标是:(a)测试命令和控制架构及硬件,(b)保持编队和重新配置控制算法,(c)通信协议和数据中继,以及(d)地球表面成像。本文详细介绍了微型卫星的设计和开发,包括编队飞行任务。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号