X-ray pulsar-based navigation method using one sensor and modified time-differenced measurement

被引:12
作者
Wang, Yidi [1 ,2 ]
Zheng, Wei [2 ]
Zhang, Dapeng [2 ]
Zhou, Qinyong [1 ,2 ,3 ]
Xin, Shijun [2 ]
机构
[1] State Key Lab Geoinformat Engn, Xian, Shaanxi, Peoples R China
[2] Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha, Hunan, Peoples R China
[3] Informat Engn Univ, Geog Spatial Informat Inst, Zhengzhou, Henan, Peoples R China
基金
中国国家自然科学基金;
关键词
X-ray pulsar navigation; systematic biases; autonomous navigation; systematic biases compensation; time-differenced measurement; SPACECRAFT;
D O I
10.1177/0954410017731440
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
X-ray pulsar-based navigation method using one sensor (XNAVO) could fix the position of satellites by sequentially observing X-ray pulsars at the cost of loading one X-ray sensor, which drops the demand on the loading capability of satellite and is feasible for practice. However, subjected to the current research status of astronomical measure and the radiation mechanism of pulsar, there are unexpected systematic biases in XNAVO, which would greatly worsen the positioning performance of XNAVO. In addition, the systematic biases compensation methods previously proposed for X-ray pulsar-based navigation using three sensors would fail when being applied to XNAVO, due to the sequential observation strategy. In order to solve the problem, this paper introduces a positioning algorithm for XNAVO based on the modified time-differenced measurement. The propagation of systematic biases is analysed, revealing the systematic biases behave a quasi-periodical variation. Thus, a modified time-differenced measurement is proposed in accordance of the quasi-periodicity. A navigation filter that propagates sigma points to generate the improved time-differenced measurement model without linearisation has been given. The results of simulation have shown that the proposed method could reduce the major impact of investigated systematic biases.
引用
收藏
页码:299 / 309
页数:11
相关论文
共 16 条
  • [1] [Anonymous], 2005, THESIS
  • [2] [Anonymous], 2000, An Introduction to the Mathematics and Methods of Astrodynamics
  • [3] Interplanetary GPS using pulsar signals
    Becker, W.
    Bernhardt, M. G.
    Jessner, A.
    [J]. ASTRONOMISCHE NACHRICHTEN, 2015, 336 (8-9) : 749 - 761
  • [4] Interplanetary spacecraft navigation using pulsars
    Deng, X. P.
    Hobbs, G.
    You, X. P.
    Li, M. T.
    Keith, M. J.
    Shannon, R. M.
    Coles, W.
    Manchester, R. N.
    Zheng, J. H.
    Yu, X. Z.
    Gao, D.
    Wu, X.
    Chen, D.
    [J]. ADVANCES IN SPACE RESEARCH, 2013, 52 (09) : 1602 - 1621
  • [5] Unscented filtering and nonlinear estimation
    Julier, SJ
    Uhlmann, JK
    [J]. PROCEEDINGS OF THE IEEE, 2004, 92 (03) : 401 - 422
  • [6] X-ray pulsar navigation method for spacecraft with pulsar direction error
    Liu, Jing
    Ma, Jie
    Tian, Jin-wen
    Kang, Zhi-wei
    White, Paul
    [J]. ADVANCES IN SPACE RESEARCH, 2010, 46 (11) : 1409 - 1417
  • [7] 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
  • [8] Effect of X-ray energy band on the X-ray pulsar based navigation
    Sun, Haifeng
    Bao, Weimin
    Fang, Haiyan
    Shen, Lirong
    Xue, Mengfan
    Li, Xiaoping
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2016, 58 : 150 - 155
  • [9] Pulse Phase Estimation of X-ray Pulsar with the Aid of Vehicle Orbital Dynamics
    Wang, Yidi
    Zheng, Wei
    [J]. JOURNAL OF NAVIGATION, 2016, 69 (02) : 414 - 432
  • [10] X-ray pulsar-based navigation using time-differenced measurement
    Wang, Yidi
    Zheng, Wei
    Sun, Shouming
    Li, Li
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2014, 36 : 27 - 35