首页> 外文会议>58th International Astronautical Congress 2007 >TETHERED NANO-SATELLITES TO OBSERVE THE SOLAR CROWN
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TETHERED NANO-SATELLITES TO OBSERVE THE SOLAR CROWN

机译:卫星状卫星观测太阳冠

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Last year the Group of Space Solar Physics at the Osservatorio Astronomico di Torino, OATo, and the AeroSpace Systems Engineering Team, ASSET, at Politecnico di Torino begun a cooperation for an ASI (Italian Space Agency) Call of Proposal on Studies of Solar System Exploration. The request that the OATo made to ASSET was the development of the capability of taking picture of both the solar crown and the solar sphere by means of simple and low cost cameras. If this was proved to be feasible, the utilization of complex optical devices could be avoided and an innovative means to perform a challenging task could be implemented. ASSET immediately realized that the simpler the payload the more complex the whole system carrying the payload would have been. However, we tackled the problem and we developed the concept of a system constituted by two low cost tethered nano-satellites, the "Detector" and the "Observer". The Observer carries one camera on-board to take pictures of the solar crown, whereas the Detector is provided with an optical device (a disk) to obscure the solar sphere and with a camera to take pictures of the solar sphere. Considering the requirement of tens of meters of distance between the camera to observe and the disk to detect, we realized that the side-length of the nano-satellites could be of about twenty centimetres. Taking into account the pointing accuracy requirement, the alignment between the two nano-satellites and the sun could be met by means of an attitude determination and control subsystem (ADCS), constituted by magnetometer, solar sensors and magnetic torques, and by means of and orbit control subsystem (OCS), constituted by positioning sensors and reaction control cold gas jets as actuators. In particular, while the ADCS is used to control the attitude of the satellites, whose cameras have to be directed towards the sun, the OCS is used to control the alignment of both satellites to the sun. The paper addresses first the requirements and then it proceeds with the development of the feasibility study of the system, thus defining both the system itself and its main subsystems. The capabilities of the system are then demonstrated through the extensive use of functional simulation of different scenarios. To conclude it is worth underlying that, notwithstanding the problems arisen both in managing the physical phenomenon and in mathematically modelling the whole system, the first results obtained are encouraging.
机译:去年,OATo的天文观测所的空间太阳物理学组和都灵的航天系统工程团队ASSET一起开始了对意大利航天局(ASI)的合作,呼吁进行关于太阳系探索研究的提案。 OATo向ASSET提出的要求是通过简单,低成本的摄像头同时拍摄太阳冠和太阳球的能力的发展。如果证明这是可行的,则可以避免使用复杂的光学设备,并可以采用创新的方法来执行具有挑战性的任务。 ASSET立即意识到,有效负载越简单,承载该有效负载的整个系统就越复杂。但是,我们解决了这个问题,并开发了由两个低成本的拴系纳米卫星“检测器”和“观察者”组成的系统的概念。观察者在船上装有一个摄像头来拍摄太阳冠的照片,而探测器则配备有光学装置(磁盘)以遮蔽太阳球,并配备有摄像头来拍摄太阳球的照片。考虑到要观察的摄像机和要检测的磁盘之间需要数十米的距离,我们意识到纳米卫星的边长可能约为20厘米。考虑到指向精度的要求,可以通过一个由磁力计,太阳传感器和磁转矩组成的姿态确定和控制子系统(ADCS)来满足两个纳米卫星与太阳之间的对准。轨道控制子系统(OCS),由定位传感器和反应控制冷气体喷嘴作为执行器组成。特别是,虽然ADCS用于控制卫星的姿态(必须将其摄像机对准太阳),但OCS用于控制两颗卫星与太阳的对准。本文首先解决了需求,然后进行了系统可行性研究的发展,从而定义了系统本身及其主要子系统。然后,通过广泛使用不同场景的功能仿真来演示系统的功能。总而言之,尽管在管理物理现象和数学建模整个系统方面都出现了问题,但值得得出的结论是令人鼓舞的。

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