{"title":"Wind-based navigation of a hot-air balloon on Titan: a feasibility study","authors":"R. Furfaro, J. Lunine, A. Elfes, K. Reh","doi":"10.1117/12.777654","DOIUrl":null,"url":null,"abstract":"Current analysis of data streamed back to Earth by the Cassini spacecraft features Titan as one of the most exciting places in the solar system. NASA centers and universities around the US, as well as the European Space Agency, are studying the possibility of sending, as part of the next mission to this giant moon of Saturn, a hot-air balloon (Montgolfier-type) for further and more in-depth exploration. The basic idea would be to design a reliable, semi-autonomous, and yet cheap Montgolfier capable of using continuous flow of waste heat from a power source to lift the balloon and sustain its altitude in the Titan environment. In this paper we study the problem of locally navigating a hot-air balloon in the nitrogen-based Titan atmosphere. The basic idea is to define a strategy (i.e. design of a suitable guidance system) that allows autonomous and semi-autonomous navigation of the balloon using the available (and partial) knowledge of the wind structure blowing on the saturnian satellite surface. Starting from first principles we determined the appropriate thermal and dynamical models describing (a) the vertical dynamics of the balloon and (b) the dynamics of the balloon moving on a vertical plane (2-D motion). Next, various non-linear fuzzy-based control strategies have been evaluated, analyzed and implemented in MATLAB to numerically simulate the capability of the system to simultaneously maintain altitude, as well as a scientifically desirable trajectory. We also looked at the ability of the balloon to perform station keeping. The results of the simulation are encouraging and show the effectiveness of such a system to cheaply and effectively perform semi-autonomous exploration of Titan.","PeriodicalId":133868,"journal":{"name":"SPIE Defense + Commercial Sensing","volume":"22 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2008-05-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"12","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"SPIE Defense + Commercial Sensing","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1117/12.777654","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 12
Abstract
Current analysis of data streamed back to Earth by the Cassini spacecraft features Titan as one of the most exciting places in the solar system. NASA centers and universities around the US, as well as the European Space Agency, are studying the possibility of sending, as part of the next mission to this giant moon of Saturn, a hot-air balloon (Montgolfier-type) for further and more in-depth exploration. The basic idea would be to design a reliable, semi-autonomous, and yet cheap Montgolfier capable of using continuous flow of waste heat from a power source to lift the balloon and sustain its altitude in the Titan environment. In this paper we study the problem of locally navigating a hot-air balloon in the nitrogen-based Titan atmosphere. The basic idea is to define a strategy (i.e. design of a suitable guidance system) that allows autonomous and semi-autonomous navigation of the balloon using the available (and partial) knowledge of the wind structure blowing on the saturnian satellite surface. Starting from first principles we determined the appropriate thermal and dynamical models describing (a) the vertical dynamics of the balloon and (b) the dynamics of the balloon moving on a vertical plane (2-D motion). Next, various non-linear fuzzy-based control strategies have been evaluated, analyzed and implemented in MATLAB to numerically simulate the capability of the system to simultaneously maintain altitude, as well as a scientifically desirable trajectory. We also looked at the ability of the balloon to perform station keeping. The results of the simulation are encouraging and show the effectiveness of such a system to cheaply and effectively perform semi-autonomous exploration of Titan.
目前卡西尼号宇宙飞船传回地球的数据分析表明,土卫六是太阳系中最令人兴奋的地方之一。美国国家航空航天局(NASA)各中心和美国各地的大学,以及欧洲航天局(European Space Agency),正在研究向这颗巨大的土星卫星发送热气球(蒙戈菲尔型)的可能性,作为下一次任务的一部分,以便进行更深入的探索。基本的想法是设计一种可靠的、半自主的、廉价的蒙哥菲,能够利用来自电源的废热持续流动来提升气球,并在土卫六环境中保持其高度。本文研究了土卫六大气层中热气球的局部导航问题。基本的想法是定义一个策略(即设计一个合适的制导系统),利用对土星卫星表面风结构的可用(和部分)知识,允许气球自主和半自主导航。从基本原理出发,我们确定了适当的热学和动力学模型来描述(a)气球的垂直动力学和(b)气球在垂直平面上运动的动力学(二维运动)。接下来,在MATLAB中对各种基于非线性模糊的控制策略进行了评估、分析和实现,以数值模拟系统同时保持高度的能力,以及科学理想的轨迹。我们还研究了气球维持空间站的能力。仿真结果令人鼓舞,显示了该系统对土卫六进行低成本、高效半自主探测的有效性。