X-ray pulsar/Doppler difference integrated navigation for deep space exploration with unstable solar spectrum

Abstract To eliminate the effects of unstable solar spectrum on the Doppler velocity measurement, a solar light Doppler difference measurement method is developed. In this method, two Doppler velocities with respect to the Sun and the Mars are measured. And their difference, which does not include the Doppler velocity bias caused by the unstable solar spectrum, is utilized as the navigation measurement. As the novel Doppler difference navigation method cannot work alone due to its accumulative position error, we combine it with the X-ray pulsar navigation method, and propose the X-ray pulsar/Doppler difference integrated navigation for deep space exploration. The simulation results demonstrate that the proposed integrated navigation method is robust to the Doppler velocity measurement bias caused by the instability of the solar spectrum effectively, and keeps the high accuracy of the pulsar/Doppler-integrated navigation system.

[1]  Jianye Liu,et al.  Augmentation of XNAV System to an Ultraviolet Sensor-Based Satellite Navigation System , 2009, IEEE Journal of Selected Topics in Signal Processing.

[2]  Du Jian Arithmetic of frequency drift and time delay between pulse profiles in XNAV , 2011 .

[3]  R. Bucy,et al.  Digital synthesis of non-linear filters , 1971 .

[4]  Jason L. Speyer,et al.  On Modeling and Pulse Phase Estimation of X-Ray Pulsars , 2010, IEEE Transactions on Signal Processing.

[5]  Jiancheng Fang,et al.  A Celestial Assisted INS Initialization Method for Lunar Explorers , 2011, Sensors.

[6]  K. Ichimoto,et al.  Hα red asymmetry of solar flares , 1984 .

[7]  Ted J. Steiner A unified vision and inertial navigation system for planetary hoppers , 2012 .

[8]  Fang Jiancheng,et al.  Analysis of Filtering Methods for Satellite Autonomous Orbit Determination Using Celestial and Geomagnetic Measurement , 2012 .

[9]  Dan Simon,et al.  Optimal State Estimation: Kalman, H∞, and Nonlinear Approaches , 2006 .

[10]  D. Pines,et al.  SPACECRAFT NAVIGATION USING X-RAY PULSARS , 2006 .

[11]  Cui Hu-tao Research on Autonomous Navigation Method of Deep Space Cruise Phase Based on the Sun Observation , 2010 .

[12]  Liu Liangdong,et al.  The use of X-ray pulsars for aiding navigation of satellites in constellations , 2009 .

[13]  Jie Ma,et al.  X-ray pulsar navigation method for spacecraft with pulsar direction error , 2010 .

[14]  Yoshifumi Sunahara,et al.  An approximate method of state estimation for nonlinear dynamical systems , 1970 .

[15]  Shengying Zhu,et al.  Observability-Based Beacon Configuration Optimization for Mars Entry Navigation , 2015 .

[16]  S. Butman,et al.  Navigation Using X-Ray Pulsars , 1981 .

[17]  Dennis W Woodfork,et al.  The Use of X-Ray Pulsars for Aiding GPS Satellite Orbit Determination , 2012 .

[18]  C. Fang,et al.  Caii K line asymmetries in two well-observed solar flares of October 18, 1990 , 1991 .

[19]  Li Li,et al.  X-ray pulsar-based navigation system with the errors in the planetary ephemerides for Earth-orbiting satellite☆ , 2013 .

[20]  Stefania Colonnese,et al.  Fast near-maximum likelihood phase estimation of X-ray pulsars , 2013, Signal Process..

[21]  Jie Ma,et al.  Doppler/XNAV-integrated navigation system using small-area X-ray sensor , 2011 .

[22]  Fang Jiancheng,et al.  Installation Direction Analysis of Star Sensors by Hybrid Condition Number , 2009, IEEE Transactions on Instrumentation and Measurement.

[23]  Jie Ma,et al.  Pulsar/CNS integrated navigation based on federated UKF , 2010 .

[24]  G. Fraser X-ray Detectors in Astronomy , 1989 .