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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:基于系绳和帆船轨迹控制系统的建模与性能分析,用于陆地科学气球任务

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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:气球系统对探索太阳系中的陆地尸体的大气表现出了很大的承诺。气球系统概念由浮出口塔和2次任务送到金星。这种系统从大气风中推进,目前无法在垂直于风的方向的方向上行进,限制了它们的勘探潜力。希望通过在垂直于风的方向上行进来修改系统轨迹的控制系统,以提高勘探潜力,以及执行维护纬度的任务。可以使用风速和密度的气球和帆系统这里讨论了产生垂直于风速的引导力的梯度。这种引导系统本质上是被动的,需要很少的动力进行致动和控制。先前证明,这种控制系统能够在Venusian气氛中产生每秒数米的引导速度。此外,该控制系统被证明能够实现对Venus的大多数纬度的足够控制。这项工作在先前的结果上建立并通过观看通过查看轨迹来通过帆系统产生引导速度的益处行星气球系统采用这种系统。首先,给出了系统模型的描述。接下来,对于金星和泰坦的气氛,轨迹控制被证明各种帆参数,例如帆尺寸和质量。这种控制的益处是通过实现给定飞行持续时间的各种兴趣的能力来示出。基于地理特征选择这些纬度,例如泰坦上的湖泊。最后,将PI控制器添加到模型中,以证明对保持和改变纬度的气球系统的基本控制。还提供了关于制度控制法的简要讨论。

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;金星;泰坦;纬度;控制;

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