宇航计测技术

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某系留气球抗风性能仿真分析

李红泉1;王雷1   

  1. 1、中国人民解放军92419部队,兴城 125106
  • 出版日期:2014-12-15 发布日期:2014-12-15
  • 作者简介:李红泉(1969-),男,高级工程师,主要研究方向:飞行器的设计与使用。

Dynamic Simulation Analysis of Wind-resistant Performance for a Tethered Balloon

LI Hong-quan1;Wang Lei1   

  1. 1、92419 Unit of PLA,Xingcheng 125106
  • Online:2014-12-15 Published:2014-12-15

摘要: 系留气球以其显著特点已应用到许多领域,今后还会有大的发展。因所处环境的风力对飞行稳定性影响较大,故抗风能力成为系统重要指标。针对无法用实验手段进行验证的空中工作姿态,一般采取计算机仿真方法进行模拟研究。介绍了系留气球的设备组成,描述了空中飞行状态,通过建立动力学模型的数学方程式,施加1-consine型离散突风模型扰动,仿真了空中球体的俯仰角和滚转角随扰动时间的关系曲线,并对结果曲线进行分析研究,以期为同型系留气球的设计方法提供某种借鉴,为浮空器使用安全提供帮助。

关键词: 系留气球, 抗风性能, 离散突风模型, 动力学仿真

Abstract: Tethered balloon is applied in many scopes by it’s characteristic, and have a great future. The ambient wind influences flight stability, so wind-resistant performance becomes the important guide line of whole system. There is no method to validate test for air attitude, and computer simulation is introduced as usual.The parts that compose the whole are introduced in this article, the flight state is described, the correlation curve is investigated between pitch angle and time and between roll angle and time by modeling dynamic equation and putting on 1-consine discrete-gust model. The numerical simulation is reference to this tethered balloon design, and is helpful to aerostat safety.

Key words: Tethered balloon, Wind-resistant performance, Discrete-gust model, Dynamic simulation