3-D Reentry Guidance with Real-Time Planning of Reference using New Analytical Solutions Based on Spectral Decomposition Method
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[1] John M. Hanson,et al. ASCENT, TRANSITION, ENTRY, AND ABORT GUIDANCE ALGORITHM DESIGN FOR THE X-33 VEHICLE , 1998 .
[2] Shuang Li,et al. Mars entry trajectory optimization using DOC and DCNLP , 2011 .
[3] J. C. Harpold,et al. Shuttle entry guidance , 1978 .
[4] W. H. T. Loh,et al. Dynamics and thermodynamics of planetary entry , 1963 .
[5] Ping Lu,et al. Onboard Generation of Three-Dimensional Constrained Entry Trajectories , 2002 .
[6] M. H. Gräßlin,et al. Ascent and reentry guidance concept based on NLP-methods , 2004 .
[7] Ping Lu,et al. Dynamic Lateral Entry Guidance Logic , 2004 .
[8] Curtis Zimmerman,et al. An Automated Method to Compute Orbital Re-Entry Trajectories with Heating Constraints , 2013 .
[9] W. H. T. Loh,et al. SOME EXACT ANALYTICAL SOLUTIONS OF PLANETARY ENTRY , 1963 .
[10] Roland N Bell. A CLOSED-FORM SOLUTION TO LIFTING REENTRY , 1965 .
[11] Wenbin Yu,et al. Guidance Scheme for Glide Range Maximization of a Hypersonic Vehicle , 2011 .
[12] Kenneth D. Mease,et al. Reduced-Order Entry Trajectory Planning for Acceleration Guidance , 2002 .
[13] F S Nyland. Hypersonic Turning with Constant Bank Angle Control , 1965 .
[14] Paul Zarchan,et al. Tactical and strategic missile guidance , 1990 .
[15] Ping Lu,et al. Gliding Guidance of High L/D Hypersonic Vehicles , 2013 .
[16] Carl D. Meyer,et al. Matrix Analysis and Applied Linear Algebra , 2000 .
[17] C. B. Cohen,et al. THE USE OF AERODYNAMIC LIFT DURING ENTRY INTO THE EARTH'S ATMOSPHERE, , 1959 .
[18] Richard W. Powell. Six-degree-of-freedom guidance and control-entry analysis of the HL-20 , 1993 .
[19] M. Cohen. Some closed form solutions to the problem of re-entry of lifting andnon-lifting vehicles , 1965 .
[20] Shuang Li,et al. Command generator tracker based direct model reference adaptive tracking guidance for Mars atmospheric entry , 2012 .
[21] Yuanqing Xia,et al. Active disturbance rejection control for drag tracking in mars entry guidance , 2014 .
[22] Greg A. Dukeman,et al. Profile-Following Entry Guidance Using Linear Quadratic Regulator Theory , 2002 .
[23] N. Vinh,et al. Hypersonic and Planetary Entry Flight Mechanics , 1980 .
[24] S. Y. Chen. THE LONGITUDINAL AND LATERAL RANGE OF HYPERSONIC GLIDE VEHICLES WITH CONSTANT BANK ANGLE , 1966 .
[25] A. J. Eggers,et al. A comparative analysis of the performance of long-range hypervelocity vehicles. , 1955 .