X-ray pulsar-based navigation semi-physical simulation experiment system

被引:11
|
作者
Su Zhe [1 ]
Xu Lu-Ping [1 ]
Wang Ting [1 ]
机构
[1] Xidian Univ, Sch Elect Engn, Xian 710071, Peoples R China
基金
中国国家自然科学基金; 国家高技术研究发展计划(863计划);
关键词
X-ray pulsar; navigation; simulation experiment system; non-homogeneous Poisson process;
D O I
10.7498/aps.60.119701
中图分类号
O4 [物理学];
学科分类号
0702 ;
摘要
For the huge costs, the space flight experiment cannot be realized in the preliminary step of X-ray pulsar based navigation (XPNAV) research. So, a kind of XPNAV semi-physical simulation experiment system is designed in this paper. This system is composed of two parts: the simulation of pulsar signal and the calculation of navigation parameters. In the first part, the time when X-ray photon arrives at the solar system barycenter is modeled by non-homogeneous Poisson process, then the output pulse of X-ray detector can be simulated by time transformation. In the second part, the navigation information included in the pulses which have been simulated in the first part can be reached by using the Delta-Correction method. This system can be used to simulate four pulsar signals simultaneously, and to study the process of signal processing and parameters calculation of XPNAV at photo level. This system has the advantage of low costs and high simulation accuracy, and provides a reference for the design of prototype in space flight experiment.
引用
收藏
页数:8
相关论文
共 16 条
  • [1] Consistent Estimation of Pulse Delay For X-ray Pulsar Based Relative Navigation
    Emadzadeh, Amir A.
    Golshan, A. Robert
    Speyer, Jason L.
    [J]. PROCEEDINGS OF THE 48TH IEEE CONFERENCE ON DECISION AND CONTROL, 2009 HELD JOINTLY WITH THE 2009 28TH CHINESE CONTROL CONFERENCE (CDC/CCC 2009), 2009, : 1488 - 1493
  • [2] MATHEWS JH, 2004, NUMERICAL METHODS US, P41
  • [3] NELSON RA, 2007, IEEE INT FREQ CONTR, P1278
  • [4] SINE INTERPOLATION OF DISCRETE PERIODIC SIGNALS
    SCHANZE, T
    [J]. IEEE TRANSACTIONS ON SIGNAL PROCESSING, 1995, 43 (06) : 1502 - 1503
  • [5] Spacecraft navigation using x-ray pulsars
    Sheikh, SI
    Pines, DJ
    Ray, PS
    Wood, KS
    Lovellette, MN
    Wolff, MT
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2006, 29 (01) : 49 - 63
  • [6] SHEIKH SI, 2005, THESIS MARYLAND U MA
  • [7] SHENG LZ, 2010, Patent No. 201001408378
  • [8] SHUAI P, 2009, CHINA SCI E, V39, P556
  • [9] SHUANI P, 2009, PRINCIPLE METHOD XRA, P341
  • [10] [孙守明 SUN Shou-ming], 2010, [宇航学报, Journal of Chinese Society of Astronautics], V31, P734