Omnidirectional Autonomous Reentry Guidance Based on 3-D Analytical Glide Formulae Considering Influence of Earth’s Rotation

[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 .