A Direct Method for Approach and Landing Trajectory Reshaping with Failure Effect Estimation

[1]  D. B. Doman,et al.  Modeling issues in footprint generation for reusable vehicles , 2003, 2003 IEEE Aerospace Conference Proceedings (Cat. No.03TH8652).

[2]  David B. Doman,et al.  Footprint Determination for Reusable Launch Vehicles Experiencing Control Effector Failures , 2002 .

[3]  David B. Doman,et al.  Dynamic Inversion-Based Adaptive/Reconfigurable Control of the X-33 on Ascent , 2002 .

[4]  M. Bolender,et al.  Nonlinear Control Allocation Using Piecewise Linear Functions , 2003 .

[5]  Michael A. Saunders,et al.  USER’S GUIDE FOR SNOPT 5.3: A FORTRAN PACKAGE FOR LARGE-SCALE NONLINEAR PROGRAMMING , 2002 .

[6]  John D. Schierman,et al.  ADAPTIVE GUIDANCE WITH TRAJECTORY RESHAPING FOR REUSABLE LAUNCH VEHICLES , 2002 .

[7]  I. Michael Ross,et al.  Towards Real-Time Computation of Optimal Controls for Nonlinear Systems , 2002 .

[8]  I. Michael Ross,et al.  A Direct Method for Solving Nonsmooth Optimal Control Problems , 2002 .

[9]  T. A. Zang,et al.  Spectral methods for fluid dynamics , 1987 .

[10]  J. Betts Survey of Numerical Methods for Trajectory Optimization , 1998 .

[11]  I. Michael Ross,et al.  Costate Estimation by a Legendre Pseudospectral Method , 1998 .

[12]  David B. Doman,et al.  Footprint calculation methods for a reusable launch vehicle , 2002, Proceedings of the 2002 American Control Conference (IEEE Cat. No.CH37301).

[13]  Eric N. Johnson,et al.  Limited authority adaptive flight control for reusable launch vehicles , 2003 .

[14]  I. Michael Ross,et al.  Second Look at Approximating Differential Inclusions , 2001 .

[15]  John D. Schierman,et al.  On-Line Trajectory Command Reshaping for Reusable Launch Vehicles , 2003 .

[16]  Gamal N. Elnagar,et al.  The pseudospectral Legendre method for discretizing optimal control problems , 1995, IEEE Trans. Autom. Control..