Analysis of Orbital Dynamic Equation in Navigation for a Mars Gravity-Assist Mission

[1]  Fang Jiancheng,et al.  Celestial Navigation Methods for Space Explorers , 2008 .

[2]  Jeffrey K. Uhlmann,et al.  New extension of the Kalman filter to nonlinear systems , 1997, Defense, Security, and Sensing.

[3]  J. E. Riedel,et al.  Interplanetary optical navigation - Voyager Uranus encounter , 1986 .

[4]  Hugh F. Durrant-Whyte,et al.  A new method for the nonlinear transformation of means and covariances in filters and estimators , 2000, IEEE Trans. Autom. Control..

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

[6]  Oliver Montenbruck,et al.  Satellite Orbits: Models, Methods and Applications , 2000 .

[7]  Wang Jiulong.  Development State and Thought of the Satellite Synthesized Electronic System , 2007 .

[8]  Fayyaz A. Lohar,et al.  Mars-Jupiter Aerogravity Assist Trajectories for High-Energy Missions , 1997 .

[9]  C. S. Christensen,et al.  Navigation of the Mariner 10 Spacecraft to Venus and Mercury , 1974 .

[10]  K. Alfriend,et al.  Adaptive Sigma Point Filtering for State and Parameter Estimation , 2004 .

[11]  Michael G. Littman,et al.  Optical navigation system , 2010 .

[12]  David Cssi Vallado.  An Analysis of State Vector Propagation Using Differing Flight Dynamics Programs , 2005 .

[13]  Vladimir A. Chobotov,et al.  Orbital Mechanics, Third Edition , 2002 .

[14]  E. M. Standish.  Present and future ephemerides: requirements and limitations , 2002 .

[15]  O. Payne,et al.  An unscented particle filter for GMTI tracking , 2004, 2004 IEEE Aerospace Conference Proceedings (IEEE Cat. No.04TH8720).

[16]  W. Folkner,et al.  The Planetary and Lunar Ephemeris DE 421 , 2009 .