Design and optimization of navigation and guidance techniques for Mars pinpoint landing: Review and prospect
暂无分享,去创建一个
[1] Jiateng Long,et al. Controllable set analysis for planetary landing under model uncertainties , 2015 .
[2] Shinji Suzuki,et al. Modified Genetic Algorithm for Constrained Trajectory Optimization , 2005 .
[3] Joseph E. Riedel,et al. Using Autonomous Navigation for Interplanetary Missions: The Validation of Deep Space 1 AutoNav , 2000 .
[4] Pingyuan Cui,et al. A beacon configuration optimization method based on Fisher information for Mars atmospheric entry , 2017 .
[5] Daniel Dueri,et al. Customized Real-Time Interior-Point Methods for Onboard Powered-Descent Guidance , 2017 .
[6] Rui Xu,et al. A Multi Sensor Based Integrated Navigation for Pin-Point Landing on Mars , 2015 .
[7] C. Ashton,et al. The Search for MH370 , 2014, Journal of Navigation.
[8] Christopher D. Karlgaard,et al. Mars Science Laboratory Entry, Descent, and Landing Trajectory and Atmosphere Reconstruction , 2013 .
[9] J. Betts. Survey of Numerical Methods for Trajectory Optimization , 1998 .
[10] Vasile Istratie. OPTIMAL SKIP ENTRY INTO ATMOSPHERE WITH MINIMUM HEAT AND CONSTRAINTS , 2000 .
[11] D. Pines,et al. SPACECRAFT NAVIGATION USING X-RAY PULSARS , 2006 .
[12] Xiuqiang Jiang,et al. Review and prospect of guidance and control for Mars atmospheric entry , 2014 .
[13] Frederick Serricchio,et al. In-flight experience of the Mars Science Laboratory Guidance, Navigation, and Control system for Entry, Descent, and Landing , 2015 .
[14] Andreas Enevold Mogensen. Real-time navigation for Mars final approach using the Mars Network , 2007 .
[15] Jarret M. Lafleur,et al. Mars Entry Bank Profile Design for Terminal State Optimization , 2011 .
[16] Robert D. Braun,et al. Statistical Entry, Descent, and Landing Performance Reconstruction of the Mars Science Laboratory , 2014 .
[17] Shengying Zhu,et al. Observability-Based Beacon Configuration Optimization for Mars Entry Navigation , 2015 .
[18] Stergios I. Roumeliotis,et al. Vision-Aided Inertial Navigation for Spacecraft Entry, Descent, and Landing , 2009, IEEE Transactions on Robotics.
[19] Adrian Sandu,et al. A Polynomial Chaos-Based Kalman Filter Approach for Parameter Estimation of Mechanical Systems , 2010 .
[20] Sanjay E. Talole,et al. Sliding Mode Observer for Drag Tracking in Entry Guidance , 2007 .
[21] Stergios I. Roumeliotis,et al. Vision‐aided inertial navigation for pin‐point landing using observations of mapped landmarks , 2007, J. Field Robotics.
[22] Alireza Khayatian,et al. Attitude estimation by divided difference filter in quaternion space , 2012 .
[23] Hutao Cui,et al. Vision-aided inertial navigation for pinpoint planetary landing , 2007 .
[24] Yanning Guo,et al. Applications of Generalized Zero-Effort-Miss/Zero-Effort-Velocity Feedback Guidance Algorithm , 2013 .
[25] Behcet Acikmese,et al. Convex programming approach to powered descent guidance for mars landing , 2007 .
[26] T. A. Ely. Optimal orbits for space constellations of Mars navigation satellites , 2000 .
[27] Ping Lu,et al. Comparison of Numerical Predictor-Corrector and Apollo Skip Entry Guidance Algorithms , 2010 .
[28] Hexi Baoyin,et al. Autonomous Navigation of Mars Probes by Combining Optical Data of Viewing Martian Moons and SST Data , 2015 .
[29] Yuanqing Xia,et al. Active disturbance rejection control for drag tracking in mars entry guidance , 2014 .
[30] Takashi Okajima,et al. The Neutron star Interior Composition ExploreR (NICER): an Explorer mission of opportunity for soft x-ray timing spectroscopy , 2012, Other Conferences.
[31] Charles D. Edwards,et al. Mars network for enabling low-cost missions , 2003 .
[32] Michèle Lavagna,et al. Pso Algorithm For Planetary Atmosphere Entry Vehicles Multidisciplinary Guidance Design , 2006 .
[33] Guangfu Ma,et al. Collision avoidance ZEM/ZEV optimal feedback guidance for powered descent phase of landing on Mars , 2017 .
[34] D. D. Morabito,et al. The Spacecraft Communications Blackout Problem Encountered during Passage or Entry of Planetary Atmospheres , 2002 .
[35] Farzin Amzajerdian,et al. Lidar systems for precision navigation and safe landing on planetary bodies , 2011, Other Conferences.
[36] G. Evensen. Sequential data assimilation with a nonlinear quasi‐geostrophic model using Monte Carlo methods to forecast error statistics , 1994 .
[37] I. Michael Ross,et al. Direct trajectory optimization by a Chebyshev pseudospectral method , 2000, Proceedings of the 2000 American Control Conference. ACC (IEEE Cat. No.00CH36334).
[38] J.A. Herath,et al. Overview of the MEDLI Project , 2008, 2008 IEEE Aerospace Conference.
[39] J. Whitaker,et al. Ensemble Square Root Filters , 2003, Statistical Methods for Climate Scientists.
[40] P. Lu,et al. Optimal Aerocapture Guidance , 2015 .
[41] Hutao Cui,et al. A new approach based on crater detection and matching for visual navigation in planetary landing , 2014 .
[42] Xiuqiang Jiang,et al. RBF neural network based second-order sliding mode guidance for Mars entry under uncertainties , 2015 .
[43] N. Vinh. Optimal trajectories in atmospheric flight , 1981 .
[44] Catherine L. Thornton,et al. Radiometric Tracking Techniques for Deep-Space Navigation , 2003 .
[45] Alexander I. Kozynchenko,et al. Analysis of predictive entry guidance for a Mars lander under high model uncertainties , 2011 .
[46] Hermann G. Matthies,et al. A deterministic filter for non-Gaussian Bayesian estimation— Applications to dynamical system estimation with noisy measurements , 2012 .
[47] Hutao Cui,et al. Constrained Numerical Predictor–Corrector Guidance for Mars Precision Landing , 2017 .
[48] David K. Geller,et al. Apollo-derived Mars precision lander guidance , 1998 .
[49] Yanning Guo,et al. Waypoint-Optimized Zero-Effort-Miss/Zero-Effort-Velocity Feedback Guidance for Mars Landing , 2013 .
[50] Raymond E. Arvidson,et al. Mars Exploration Rover mission , 2003 .
[51] Larry H. Matthies,et al. Design Through Operation of an Image-Based Velocity Estimation System for Mars Landing , 2007, International Journal of Computer Vision.
[52] R. H. Bishop,et al. Robust entry navigation using hierarchical filter architectures regulated with gating networks , 2001 .
[53] P. Graven,et al. AAS 08-054 1 XNAV FOR DEEP SPACE NAVIGATION , 2008 .
[54] Kenneth D. Mease,et al. Trajectory Tracking and Online Replanning for Mars Entry , 2016 .
[55] Shengying Zhu,et al. An innovative navigation scheme of powered descent phase for Mars pinpoint landing , 2014 .
[56] Shengying Zhu,et al. Orbit optimization of Mars orbiters for entry navigation: From an observability point of view , 2015 .
[57] Namhoon Cho,et al. Three-Dimensional Nonlinear Differential Geometric Path-Following Guidance Law , 2015 .
[58] Geethu Lisba Jacob,et al. Mars Entry Mission Bank Profile Optimization , 2014 .
[59] Fabrizio Pirondini,et al. A New Approach to the Design of Navigation Constellations around MARS: The MARCO POLO Evolutionary System , 2006 .
[60] Shengying Zhu,et al. On the observability of Mars entry navigation using radiometric measurements , 2014 .
[61] Robert H. Bishop,et al. Multi-model Navigation with Gating Networks for Mars Entry Precision Landing , 2004 .
[62] R. Manning,et al. Mars exploration entry, descent and landing challenges , 2006, 2006 IEEE Aerospace Conference.
[63] Todd Ely,et al. Altair Navigation During Trans-Lunar Cruise, Lunar Orbit, Descent and Landing , 2010 .
[64] Shengying Zhu,et al. Real-time Navigation for Mars Final Approach Using X-ray Pulsars , 2013 .
[65] C. A. Kluever,et al. Entry Guidance Performance for Mars Precision Landing , 2008 .
[66] Louis A. D'Amario,et al. Mars exploration rovers navigation results , 2004 .
[67] Huimin Fu,et al. Multiple Model Adaptive Rank Estimation for Integrated Navigation During Mars Entry , 2016, Journal of Navigation.
[68] Jason L. Speyer,et al. Relative Navigation Between Two Spacecraft Using X-ray Pulsars , 2011, IEEE Transactions on Control Systems Technology.
[69] Xiuqiang Jiang,et al. High-precision Mars Entry Integrated Navigation Under Large Uncertainties , 2014 .
[70] Marco B. Quadrelli,et al. Guidance Navigation and Control Technology Assessment for Future Planetary Science Missions , 2013 .
[71] Fernando Abilleira,et al. Mars Science Laboratory Interplanetary Navigation , 2014 .
[72] F. Amzajerdian,et al. Doppler lidar sensor for precision landing on the Moon and Mars , 2012, 2012 IEEE Aerospace Conference.
[73] Anil V. Rao,et al. GPOPS-II , 2014, ACM Trans. Math. Softw..
[74] Hermann G. Matthies,et al. Sampling-free linear Bayesian updating of model state and parameters using a square root approach , 2013, Comput. Geosci..
[75] Amitabh Saraf,et al. Design and Evaluation of an Acceleration Guidance Algorithm for Entry , 2003 .
[76] Kenneth D. Mease,et al. Feasible Trajectory Generation for Atmospheric Entry Guidance , 2007 .
[77] Roberto Furfaro,et al. Mars Atmospheric Entry Guidance via Multiple Sliding Surface Guidance for Reference Trajectory Tracking , 2012 .
[78] Chen Gang,et al. Genetic algorithm optimization of RLV reentry trajectory , 2005 .
[79] H. Carvalho,et al. Optimal nonlinear filtering in GPS/INS integration , 1997, IEEE Transactions on Aerospace and Electronic Systems.
[80] Joel Benito Manrique. Advances in spacecraft atmospheric entry guidance , 2010 .
[81] Pingyuan Cui,et al. Optimal landing site selection based on safety index during planetary descent , 2017 .
[82] Arthur E. Bryson,et al. Applied Optimal Control , 1969 .
[83] Charles D. Edwards,et al. The Electra proximity link payload for Mars relay telecommunications and navigation , 2003 .
[84] Christof Büskens,et al. Real-Time Atmospheric Entry Trajectory Computation Using Parametric Sensitivities , 2016 .
[85] Robert D. Braun,et al. Rapid Entry Corridor Trajectory Optimization for Conceptual Design , 2010 .
[86] Kyu-Hong Choi,et al. Satellite orbit determination using a batch filter based on the unscented transformation , 2010 .
[87] A. Rao,et al. Performance Optimization of a Maneuvering Re-Entry Vehicle Using a Legendre Pseudospectral Method , 2002 .
[88] Ping Lu,et al. Comparison of Fully Numerical Predictor-Corrector and Apollo Skip Entry Guidance Algorithms , 2012 .
[89] Shyam Bhaskaran,et al. Mars approach navigation using Mars network based doppler tracking , 2002 .
[90] S. Sheikh. The Use Of Variable Celestial X-ray Sources For Spacecraft Navigation , 2005 .
[91] G. Downs. Interplanetary navigation using pulsating radio sources , 1974 .
[92] Anil V. Rao,et al. ENTRY TRAJECTORY TRACKING LAW VIA FEEDBACK LINEARIZATION , 1998 .
[93] J. C. Harpold,et al. Space Shuttle entry guidance performance results , 1983 .
[94] Shuang Li,et al. Innovative Mars entry integrated navigation using modified multiple model adaptive estimation , 2014 .
[95] Rajesh Arora. Reentry Trajectory Optimization: Evolutionary Approach , 2002 .
[96] Roberto Furfaro,et al. Non-linear Sliding Guidance algorithms for precision lunar landing , 2011 .
[97] Taishan Lou,et al. Robust Mars Atmospheric Entry Integrated Navigation based on Parameter Sensitivity , 2015, ArXiv.
[98] Raktim Bhattacharya,et al. Polynomial Chaos-Based Analysis of Probabilistic Uncertainty in Hypersonic Flight Dynamics , 2010 .
[99] Yuanqing Xia,et al. Mars atmospheric entry guidance for reference trajectory tracking , 2015 .
[100] Juan R. Cruz,et al. Entry, Descent, and Landing Performance of the Mars Phoenix Lander , 2008 .
[101] Robert D. Braun. The Mars Science Laboratory Entry, Descent, and Landing System , 2014 .
[102] David Benson,et al. A Gauss pseudospectral transcription for optimal control , 2005 .
[103] Eberhard Gill,et al. Relative state estimation and observability for formation flying satellites in the presence of sensor noise , 2010 .
[104] Robert D. Braun,et al. Guidance, Navigation, and Control System Performance Trades for Mars Pinpoint Landing , 2010 .
[105] Edward C. Wong,et al. Guidance and Control Design for Hazard Avoidance and Safe Landing on Mars , 2006 .
[106] Yuanqing Xia,et al. Improved ZEM/ZEV feedback guidance for Mars powered descent phase , 2014 .
[107] I. Michael Ross,et al. Costate Estimation by a Legendre Pseudospectral Method , 1998 .
[108] Robert H. Bishop,et al. MARS ENTRY NAVIGATION FROM EKF PROCESSING OF BEACON DATA , 2000 .
[109] Yuanqing Xia,et al. Mars Entry Navigation With Uncertain Parameters Based on Desensitized Extended Kalman Filter , 2015, IEEE Transactions on Industrial Informatics.
[110] Donn B. Kirk,et al. Aerodynamic Behavior of the Viking Entry Vehicle: Ground Test and Flight Results , 1978 .
[111] Jean Francois Levesque,et al. Innovative Navigation Schemes for State and Parameter Estimation During Mars Entry , 2007 .
[112] E. Glenn Lightsey,et al. Expected EDL navigation performance with spacecraft to spacecraft radiometric data , 2005 .
[113] Gavin Mendeck,et al. Guidance Design for Mars Smart Landers Using the Entry Terminal Point Controller , 2002 .
[114] Ping Lu,et al. Entry Guidance: A Unified Method , 2014 .
[115] Fu Huimin,et al. RANK FILTER METHOD , 2014 .
[116] Liu Zhang,et al. MCAV/IMU integrated navigation for the powered descent phase of Mars EDL , 2010 .
[117] E. Glenn Lightsey,et al. Real-Time Navigation for Mars Missions Using the Mars Network , 2008 .
[118] Pingyuan Cui,et al. A polynomial chaos based square-root Kalman filter for Mars entry navigation , 2016 .
[119] Darren Baird,et al. Mars Exploration Rover Cruise Orbit Determination , 2004 .
[120] A.E. Johnson,et al. Overview of Terrain Relative Navigation Approaches for Precise Lunar Landing , 2008, 2008 IEEE Aerospace Conference.
[121] S. Ploen,et al. A Powered Descent Guidance Algorithm for Mars Pinpoint Landing , 2005 .
[122] Marvin K. Simon,et al. Autonomous Software-Defined Radio Receivers for Deep Space Applications , 2006 .
[123] Prasun N. Desai,et al. Mars exploration rovers entry, descent, and landing trajectory analysis , 2004 .
[124] Renato Zanetti. Advanced navigation algorithms for precision landing , 2007 .
[125] Pingyuan Cui,et al. X-ray pulsars/Doppler integrated navigation for Mars final approach , 2016 .
[126] Keith C. Gendreau,et al. X-ray pulsar navigation algorithms and testbed for SEXTANT , 2015, 2015 IEEE Aerospace Conference.
[127] Benjamin L. Pence,et al. A maximum likelihood approach to recursive polynomial chaos parameter estimation , 2010, Proceedings of the 2010 American Control Conference.
[128] Colin R. McInnes. Gravity Turn Descent with Quadratic Air Drag , 1997 .
[129] Brian D. Pollard,et al. A Radar Terminal Descent Sensor for the Mars Science Laboratory mission , 2009, 2009 IEEE Aerospace conference.
[130] Nesrin Sarigul-Klijn,et al. Survey of planetary entry guidance algorithms , 2014 .
[131] D. J. Bell,et al. Mars network: a Mars orbiting communications and navigation satellite constellation , 2000, 2000 IEEE Aerospace Conference. Proceedings (Cat. No.00TH8484).
[132] Michael J. Grant,et al. Mars Science Laboratory Entry Optimization Using Particle Swarm Methodology , 2007 .
[133] Behrouz Ebrahimi,et al. Optimal sliding-mode guidance with terminal velocity constraint for fixed-interval propulsive maneuvers , 2008 .
[134] Edward C. Wong,et al. Autonomous guidance and control design for hazard avoidance aand safe landing on Mars , 2002 .
[135] Andrew E. Johnson,et al. Analysis and Testing of a LIDAR-Based Approach to Terrain Relative Navigation for Precise Lunar Landing , 2011 .
[136] A. Vasavada,et al. Reconstruction of Atmospheric Properties from Mars Science Laboratory Entry, Descent, and Landing , 2014 .
[137] Jarret M. Lafleur. Trading Robustness Requirements in Mars Entry Trajectory Design , 2009 .
[138] Gavin F. Mendeck,et al. Entry Guidance Design and Postflight Performance for 2011 Mars Science Laboratory Mission , 2014 .
[139] Dongbin Xiu,et al. A generalized polynomial chaos based ensemble Kalman filter with high accuracy , 2009, J. Comput. Phys..
[140] Martin Cornelius Heyne. Spacecraft precision entry navigation using an adaptive sigma point Kalman filter bank , 2007 .
[141] G. Evensen. Sampling strategies and square root analysis schemes for the EnKF , 2004 .
[142] Farzin Amzajerdian,et al. LIDAR-Aided Inertial Navigation with Extended Kalman Filtering for Pinpoint Landing , 2009 .
[143] R. V. Jategaonkar,et al. Aerodynamic parameter estimation from flight data applying extended and unscented Kalman filter , 2006 .
[144] S. Butman,et al. Navigation Using X-Ray Pulsars , 1981 .
[145] Behçet Açikmese,et al. Constrained Reachability and Controllability Sets for Planetary Precision Landing via Convex Optimization , 2015 .
[146] Shuang Li,et al. Mars entry trajectory optimization using DOC and DCNLP , 2011 .
[147] B. Jai,et al. The Mars reconnaissance orbiter mission , 2005, 2004 IEEE Aerospace Conference Proceedings (IEEE Cat. No.04TH8720).
[148] K. Lau,et al. AN INNOVATIVE DEEP SPACE APPLICATION OF GPS TECHNOLOGY FOR FORMATION FLYING SPACECRAFT , 1996 .
[149] Kuang-Yang Tu,et al. Drag-based predictive tracking guidance for Mars precision landing , 1998 .
[150] Kuang-Yang Tu,et al. Drag-Based Predictive Tracking Guidance for Mars Precision Landing , 1998 .
[151] Christopher N. D'Souza,et al. AN OPTIMAL GUIDANCE LAW FOR PLANETARY LANDING , 1997 .
[152] O. Romberg,et al. Mars and Moon exploration passing through the European Precision Landing GNC Test Facility , 2008 .
[153] Hutao Cui,et al. Mars Atmospheric Entry Guidance Using a Sensitivity Method , 2017, IEEE Transactions on Aerospace and Electronic Systems.
[154] Colin R. McInnes. DIRECT ADAPTIVE CONTROL FOR GRAVITY-TURN DESCENT , 1999 .
[155] Pingyuan Cui,et al. A Novel Trajectory Optimization Method for Mars Atmospheric Entry , 2015 .
[156] Pingyuan Cui,et al. An Observability-Based Trajectory Optimization Considering Disturbance for Atmospheric Entry , 2016 .
[157] Ping Lu,et al. Regulation About Time-Varying Trajectories: Precision Entry Guidance Illustrated , 1999 .
[158] T. Singh,et al. Efficient particle filtering for road-constrained target tracking , 2005 .
[159] Joel Benito,et al. Reachable and Controllable Sets for Planetary Entry and Landing , 2010 .