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A simplified metric for formulating and assessing elastic launch dynamics

机译:用于制定和评估弹性发射动力学的简化指标

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摘要

Elastic launch devices are widely used in aviation and aerospace, whereas the accurate assessment and practical control of their dynamic performance are often complicated. We propose and validate a metric approach to simplify the launch dynamics, regardless of unstable elastic parameters and various device distributions. The nonlinear relationship between main separation parameters and elastic potential energy is derived and quantified by the defined metric, which achieves the effective assessment and control of launch process in a simple way. The metric theory is proved by the actual ground tests of a typical launch using the pre-compressed spring devices. In addition, the approach has been successfully applied to evaluate and optimize TianTuo-1 satellite launch, reflecting small errors and easy operation in practical use.
机译:弹性发射装置广泛用于航空和航天,而对其动态性能的准确评估和实际控制通常很复杂。我们提出并验证一种度量方法,以简化发射动力学,而不考虑不稳定的弹性参数和各种设备分布。通过定义的度量推导和量化了主要分离参数与弹性势能之间的非线性关系,从而以简单的方式实现了对发射过程的有效评估和控制。公制理论通过使用预压缩弹簧装置的典型发射的实际地面测试得到证明。此外,该方法已成功地应用于评估和优化天T一号卫星的发射,反映出较小的误差和在实际使用中易于操作。

著录项

  • 来源
    《Acta astronautica》 |2014年第sepaaocta期|151-155|共5页
  • 作者单位

    College of Aerospace Science and Engineering, National University of Defense Technology, 410073, China;

    College of Aerospace Science and Engineering, National University of Defense Technology, 410073, China;

    College of Aerospace Science and Engineering, National University of Defense Technology, 410073, China;

    College of Aerospace Science and Engineering, National University of Defense Technology, 410073, China;

  • 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

    Launch dynamics; Separation process; Metric; Elastic potential energy; TianTuo-1 satellite;

    机译:发射动力;分离过程;公制弹性势能;天陀一号卫星;

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