首页> 外文会议>International Astronautical Congress(IAC2006); 20061002-06; Valencia(ES) >Stability and Control Response of Spinning Solar Sail-craft containing A Huge Membrane
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Stability and Control Response of Spinning Solar Sail-craft containing A Huge Membrane

机译:大型膜旋转太阳帆飞行器的稳定性和控制响应

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At the Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency(JAXA), Spinning Solar Sail-craft is proposed and examined the possibility. In August 2006, a membrane of 20 [m] in diameter was deployed statically by using a flying balloon. The size of membrane is the largest in the world, furthermore, to deploy statically is the first achievement in the world. This paper shows the experiment apparatus and the results. Additionally, numerical simulation is used to analyze the behavior of the membrane. The deployment of membrane is divided first stage and second stage. At first stage deployment, the membrane deploys dynamically because the accident occurs. However, the deployment is successful. At second stage deployment, the membrane deploys statically and finally forms square-shape. The numerical simulation accords with the behavior of membrane. The membrane has the inclination by gravity, so the experiment can examine the out-of-motion of the membrane. And the membrane is affected by air drag, the contortion of the membrane is also examined. As a conclusion, to deploy a membrane of 20[m] in diameter statically is the first achievement in the world, and to analyze the behavior of the membrane is meaningful for the realization of Solar Sail-craft.
机译:在日本航空航天局(JAXA)的太空与宇航科学研究所(ISAS)中,提出了旋转太阳帆飞行器并研究了这种可能性。 2006年8月,使用飞行气球将直径为20 [m]的膜静态展开。膜的尺寸是世界上最大的,而且,静态部署是世界上的第一个成就。本文展示了实验装置和结果。此外,数值模拟用于分析膜的行为。膜的部署分为第一阶段和第二阶段。在第一阶段部署中,由于发生事故,膜会动态部署。但是,部署成功。在第二阶段展开时,膜会静态展开,最后形成方形。数值模拟符合膜的性能。膜片因重力而倾斜,因此实验可以检查膜片的运动状态。并且膜受到空气阻力的影响,还检查了膜的扭曲。结论是,静态部署直径为20 [m]的膜是世界上的第一项成就,分析膜的行为对于实现太阳帆飞行器具有重要意义。

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