首页> 外文学位 >Representation of Unknown and Unmodeled Space Events for Satellites: Characteristics and Applications.
【24h】

Representation of Unknown and Unmodeled Space Events for Satellites: Characteristics and Applications.

机译:卫星未知和未建模空间事件的表示:特性和应用。

获取原文
获取原文并翻译 | 示例

摘要

A new way of representing unknown and unmodeled space events (USEs) with Thrust-Fourier-Coefficients (TFCs) is introduced and its applications to satellite orbit determination (OD) and event detection are studied. A USE is regarded as an event due to unknown changes of force model caused by unplanned maneuvers, unknown deployment, collision, or some other drastic change in space environment. A satellite's motion under USEs, transitioning between two arbitrary orbit states, can be represented as an equivalent orbital maneuver connecting those two states by applying the Fourier series representation of perturbing accelerations. This event representation with TFCs rigorously provides a unique control law that can generate the given secular behavior of a satellite due to a USE. This technique enables us to facilitate the analytical propagation of orbit information across a USE, which allows for the usage of an existing pre-event orbit solution to compute a post-event orbit solution. By directly appending TFCs and the represented event dynamics to a regular OD filter, the modified filter using TFCs is able to blend post-event tracking data to improve a post-event orbit solution in the absence of a dynamics model of USE. Case studies with simulated tracking data show that the event representation using TFCs helps to maintain OD across a period of USEs. In addition, when there is measurement data available during USEs, a modified sequential filter with TFCs is able to detect the onset and the termination time of an event. This event representation-based OD and event detection distinguishes itself from other approaches in that it does not rely on any assumption or a priori information of a USE. This generic approach enables us to fit tracking data in real time and therefore to maintain a satellite tracking in the presence of USEs. This method has the advantage of avoiding the difficulty of manual parameter tuning and, thus, is able to provide more accurate post-event OD solution with a single OD filter.
机译:介绍了一种用推力-傅立叶系数(TFC)表示未知和未建模空间事件(USE)的新方法,并研究了其在卫星轨道确定(OD)和事件检测中的应用。由于计划外的操纵,未知的部署,碰撞或太空环境中的其他剧烈变化所引起的力模型的未知变化,USE被视为事件。通过应用扰动加速度的傅里叶级数表示,在USEs下在两个任意轨道状态之间转换的卫星运动可以表示为连接这两个状态的等效轨道操纵。带有TFC的事件表示法严格地提供了一种独特的控制规律,该规律可因使用而产生卫星的给定长期行为。这项技术使我们能够促进在USE中进行轨道信息的分析传播,从而允许使用现有的事件前轨道解决方案来计算事件后轨道解决方案。通过直接将TFC和所表示的事件动态附加到常规OD过滤器,使用TFC的修改后的过滤器能够混合事件后跟踪数据,以在没有USE动力学模型的情况下改善事件后轨道解决方案。带有模拟跟踪数据的案例研究表明,使用TFC进行事件表示有助于在整个USE期间保持OD。此外,当在USE期间有可用的测量数据时,带有TFC的经过修改的顺序滤波器能够检测事件的开始和终止时间。这种基于事件表示的OD和事件检测将其自身与其他方法区分开来,因为它不依赖于USE的任何假设或先验信息。这种通用方法使我们能够实时拟合跟踪数据,因此可以在存在使用情况的情况下保持卫星跟踪。这种方法的优点是避免了手动参数调整的困难,因此能够通过单个OD过滤器提供更准确的事后OD解决方案。

著录项

  • 作者

    Ko, Hyun Chul.;

  • 作者单位

    University of Colorado at Boulder.;

  • 授予单位 University of Colorado at Boulder.;
  • 学科 Aerospace engineering.;Systems science.;Mechanical engineering.
  • 学位 Ph.D.
  • 年度 2015
  • 页码 173 p.
  • 总页数 173
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号