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首页> 外文期刊>Acta astronautica >Modelling and performance analysis of a tether and sail-based trajectory control system for extra-terrestrial scientific balloon missions
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Modelling and performance analysis of a tether and sail-based trajectory control system for extra-terrestrial scientific balloon missions

机译:基于系绳和帆的轨迹控制系统的建模和性能分析,用于地面外科学气球飞行任务

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摘要

Balloon systems show great promise for exploring the atmospheres of extra-terrestrial bodies in the solar system. The balloon system concept was demonstrated by the aerostats aboard the Vega 1 and 2 missions sent to Venus. Such systems glean propulsion from atmospheric winds, and at present are unable to travel in a direction perpendicular to the direction of the wind, limiting their exploration potential. A control system capable of modifying the system trajectory by traveling in a direction perpendicular to the direction of the wind is desired to increase exploration potential as well as to perform tasks such as maintaining latitude.A balloon and sail system which can use wind velocity and density gradients to produce a guiding force perpendicular to the velocity of the wind is discussed here. Such a guidance system is passive in nature and requires little power for actuation and control. It was previously demonstrated that such a control system is capable of generating guiding velocities of several meters per second within the Venusian atmosphere. Furthermore, this control system was shown to be capable of achieving sufficient control for the majority of the latitudes on Venus.This work builds on previous results and demonstrates the benefits of being able to generate guiding velocities via a sail system by viewing the trajectories taken by planetary balloon systems employing such a system. First, a description of the system model is given. Next, for the atmospheres of Venus and Titan, trajectory control is demonstrated for various sail parameters, such as sail size and mass. The benefit of such control is shown by the ability to achieve various latitudes of interest for a given flight duration. These latitudes are chosen based on geographic features, such as lakes on Titan. Finally, a PI controller is added to the model to demonstrate rudimentary control of the balloon system for maintaining and changing latitudes. A brief discussion regarding the control law of the system is also provided.
机译:气球系统显示出探索太阳系中地球外物体大气的巨大希望。气球系统的概念由发送给金星的Vega 1和2任务上的浮空器演示。这样的系统收集来自大气的推进力,并且目前不能在垂直于风的方向上行进,从而限制了其勘探潜力。需要一种能够通过在垂直于风向的方向上行进来改变系统轨迹的控制系统,以增加勘探潜力并执行诸如维持纬度之类的任务。气球和帆系统可以利用风速和密度这里讨论了产生垂直于风速的引导力的梯度。这样的引导系统本质上是被动的,并且需要很少的动力来进行致动和控制。先前已经证明,这样的控制系统能够在金星大气中产生每秒几米的引导速度。此外,该控制系统已被证明能够对金星的大部分纬度进行充分的控制。这项工作是建立在先前结果的基础之上的,并展示了能够通过查看航行轨迹而通过帆系统产生引导速度的好处。采用这种系统的行星气球系统。首先,给出系统模型的描述。接下来,针对金星和土卫六的大气层,演示了针对各种风帆参数(例如风帆大小和质量)的轨迹控制。对于给定的飞行持续时间,获得各种感兴趣的纬度的能力表明了这种控制的好处。这些纬度是根据地理特征(例如泰坦上的湖泊)选择的。最后,将PI控制器添加到模型中,以演示气球系统的基本控制,以维持和更改纬度。还简要讨论了系统的控制规律。

著录项

  • 来源
    《Acta astronautica》 |2019年第7期|527-537|共11页
  • 作者单位

    North Carolina State Univ, Dept Mech & Aerosp Engn, 911 Oval Dr, Raleigh, NC 27695 USA;

    North Carolina State Univ, Dept Mech & Aerosp Engn, 911 Oval Dr, Raleigh, NC 27695 USA;

    North Carolina State Univ, Dept Mech & Aerosp Engn, 911 Oval Dr, Raleigh, NC 27695 USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Balloon; Sail; Venus; Titan; Latitude; Control;

    机译:气球;帆船;金星;泰坦;纬度;控制;

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