An innovative navigation scheme of powered descent phase for Mars pinpoint landing
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[1] S. Ploen,et al. Performance trades for Mars pinpoint landing , 2006, 2006 IEEE Aerospace Conference.
[2] Yanning Guo,et al. Waypoint-Optimized Zero-Effort-Miss/Zero-Effort-Velocity Feedback Guidance for Mars Landing , 2013 .
[3] Aron A. Wolf,et al. A Comparison of Powered Descent Guidance Laws for Mars Pinpoint Landing. , 2006 .
[4] Xiangyu Huang,et al. GNC system scheme for lunar soft landing spacecraft , 2008 .
[5] Canuto Enrico,et al. Disturbance rejection in space applications: Problems and solutions , 2011, Proceedings of the 30th Chinese Control Conference.
[6] M. Psiaki. Backward-Smoothing Extended Kalman Filter , 2005 .
[7] Christopher N. D'Souza,et al. AN OPTIMAL GUIDANCE LAW FOR PLANETARY LANDING , 1997 .
[8] J. Junkins,et al. Optimal Estimation of Dynamic Systems , 2004 .
[9] E.C. Wong,et al. Guidance and Control Design for Powered Descent and Landing on Mars , 2007, 2007 IEEE Aerospace Conference.
[10] Allan R. Klumpp,et al. Apollo lunar descent guidance , 1974, Autom..
[11] Simon Lacroix,et al. Visual Landmark Constellation matching for spacecraft pinpoint landing , 2009 .
[12] Premkumar R. Menon,et al. Mars Reconnaissance Orbiter Navigation Strategy for Mars Science Laboratory Entry, Descent and Landing Telecommunication Relay Support , 2012 .
[13] Sang-Young Park,et al. Onboard orbit determination using GPS observations based on the unscented Kalman filter , 2010 .
[14] A. Chen,et al. Mars Science Laboratory Entry, Descent, and Landing System Overview , 2008, 2008 IEEE Aerospace Conference.
[15] J. Balaram,et al. Mars Science Laboratory Simulations for Entry, Descent, and Landing , 2006 .
[16] Klaus Janschek,et al. Performance Analysis for Visual Planetary Landing Navigation Using Optical Flow and DEM Matching , 2006 .
[17] Hutao Cui,et al. A new approach based on crater detection and matching for visual navigation in planetary landing , 2014 .
[18] Farzin Amzajerdian,et al. LIDAR-Aided Inertial Navigation with Extended Kalman Filtering for Pinpoint Landing , 2009 .
[19] E. Canuto,et al. Planetary landing: Modelling and control of the propulsive descent , 2012, Proceedings of the 31st Chinese Control Conference.
[20] Hang Guo,et al. Kalman filtering for GPS/magnetometer integrated navigation system , 2010 .
[21] R. Manning,et al. Mars Exploration Entry, Descent, and Landing Challenges , 2007 .
[22] Liu Zhang,et al. MCAV/IMU integrated navigation for the powered descent phase of Mars EDL , 2010 .
[23] Curtis W. Chen,et al. Phoenix Landing Radar Heatshield Anomaly , 2011 .
[24] Brian D. Pollard,et al. A Radar Terminal Descent Sensor for the Mars Science Laboratory mission , 2009, 2009 IEEE Aerospace conference.
[25] F. Ham,et al. Observability, Eigenvalues, and Kalman Filtering , 1983, IEEE Transactions on Aerospace and Electronic Systems.
[26] F. Amzajerdian,et al. Doppler lidar sensor for precision landing on the Moon and Mars , 2012, 2012 IEEE Aerospace Conference.