Omnidirectional Autonomous Reentry Guidance Based on 3-D Analytical Glide Formulae Considering Influence of Earth’s Rotation
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[1] C. B. Cohen,et al. THE USE OF AERODYNAMIC LIFT DURING ENTRY INTO THE EARTH'S ATMOSPHERE, , 1959 .
[2] Ping Lu,et al. Entry Guidance: A Unified Method , 2014 .
[3] M. Cohen. Some closed form solutions to the problem of re-entry of lifting andnon-lifting vehicles , 1965 .
[4] Rui Zhou,et al. Reentry trajectory optimization for hypersonic vehicle satisfying complex constraints , 2013 .
[5] Wanchun Chen,et al. Longitudinal characteristics of steady glide trajectory for hypersonic vehicle , 2015, 2015 International Conference on Control, Automation and Information Sciences (ICCAIS).
[6] Ping Lu,et al. Onboard Generation of Three-Dimensional Constrained Entry Trajectories , 2002 .
[7] R. V. Jategaonkar,et al. Aerodynamic Parameter Estimation from Flight Data Applying Extended and Unscented Kalman Filter , 2010 .
[8] Yu Xie,et al. Highly constrained entry trajectory generation , 2013 .
[9] Xiaodong Liu,et al. Guidance law against maneuvering targets with intercept angle constraint. , 2014, ISA transactions.
[10] Honglun Wang,et al. Active disturbance rejection based trajectory linearization control for hypersonic reentry vehicle with bounded uncertainties. , 2015, ISA transactions.
[11] A. J. Eggers,et al. Performance of Long Range Hypervelocity Vehicles , 1957 .
[12] Richard W. Powell. Six-degree-of-freedom guidance and control-entry analysis of the HL-20 , 1993 .
[13] Wanchun Chen,et al. Trajectory-Shaping Guidance with final speed and load factor constraints. , 2015, ISA transactions.
[14] S. Y. Chen. THE LONGITUDINAL AND LATERAL RANGE OF HYPERSONIC GLIDE VEHICLES WITH CONSTANT BANK ANGLE , 1966 .
[15] A. J. Eggers,et al. A comparative analysis of the performance of long-range hypervelocity vehicles. , 1955 .
[16] F S Nyland. Hypersonic Turning with Constant Bank Angle Control , 1965 .
[17] Greg A. Dukeman,et al. Profile-Following Entry Guidance Using Linear Quadratic Regulator Theory , 2002 .
[18] Rui Zhou,et al. Pigeon-inspired optimization applied to constrained gliding trajectories , 2015 .
[19] Curtis Zimmerman,et al. An Automated Method to Compute Orbital Re-Entry Trajectories with Heating Constraints , 2013 .
[20] Wanchun Chen,et al. Entry guidance with real-time planning of reference based on analytical solutions , 2015 .
[21] Rui Zhang,et al. Novel prescribed performance neural control of a flexible air-breathing hypersonic vehicle with unknown initial errors. , 2015, ISA transactions.
[22] Zhongke Shi,et al. Direct neural discrete control of hypersonic flight vehicle , 2012 .
[23] Kenneth D. Mease,et al. Reduced-Order Entry Trajectory Planning for Acceleration Guidance , 2002 .
[24] Qun Zong,et al. Integrated guidance and control for reusable launch vehicle in reentry phase , 2015 .
[25] Guojian Tang,et al. Entry trajectory planning based on three-dimensional acceleration profile guidance , 2016 .
[26] W. H. T. Loh,et al. Dynamics and thermodynamics of planetary entry , 1963 .
[27] J. Douglas Faires,et al. Numerical Analysis , 1981 .
[28] John M. Hanson,et al. ASCENT, TRANSITION, ENTRY, AND ABORT GUIDANCE ALGORITHM DESIGN FOR THE X-33 VEHICLE , 1998 .
[29] Youan Zhang,et al. Sliding mode control based impact angle control guidance considering the seeker׳s field-of-view constraint. , 2016, ISA transactions.
[30] M. H. Gräßlin,et al. Ascent and reentry guidance concept based on NLP-methods , 2004 .
[31] W. H. T. Loh,et al. SOME EXACT ANALYTICAL SOLUTIONS OF PLANETARY ENTRY , 1963 .
[32] Roland N Bell. A CLOSED-FORM SOLUTION TO LIFTING REENTRY , 1965 .
[33] Wenbin Yu,et al. Guidance Scheme for Glide Range Maximization of a Hypersonic Vehicle , 2011 .