首页> 外文会议>International conference on computer and network technology >Simulate and Model on X-ray pulsar navigation for spacecraft
【24h】

Simulate and Model on X-ray pulsar navigation for spacecraft

机译:航天器X射线脉冲星导航的仿真和建模

获取原文

摘要

X-ray pulsar navigation (XPNAV) is one of the most attractive autonomous navigation methods for spacecraft utilizing accurate timing.The principle,time transfer model and simulation of this navigation method are mentioned in this paper.Extended Kalman filter is also used to estimate vehicle's position and velocity in inertia! frame.Three kinds of X-ray detector schemes are present,as single fixed detector scheme,single servo detector scheme,and multi-detector scheme.The numerical simulations show that the accuracy of the orbit determination using XPNAV is better than 10m,and the single detector servo assembling scheme is more suitable for the future missions and flying experiments according to the navigation accuracy and equipment weight.
机译:X射线脉冲星导航(XPNAV)是利用精确定时的航天器最有吸引力的自主导航方法之一。本文介绍了这种导航方法的原理,时间传递模型和仿真。惯性位置和速度!提出了三种X射线探测器方案,分别是单固定探测器方案,单伺服探测器方案和多探测器方案。数值模拟表明,用XPNAV确定轨道的精度优于10m,并且根据导航精度和设备重量,单探测器伺服组装方案更适合将来的任务和飞行实验。

著录项

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