Rapid Trajectory Optimization Using Computational Intelligence for Guidance and Conceptual Design of Multistage Space Launch Vehicles

[1]  M. Stein Large sample properties of simulations using latin hypercube sampling , 1987 .

[2]  Takeshi Tsuchiya,et al.  Spaceplane Trajectory Optimization with Vehicle Size Analysis , 1998 .

[3]  Tapabrata Ray,et al.  Swarm algorithm for single- and multiobjective airfoil design optimization , 2004 .

[4]  Takeshi Tsuchiya,et al.  Optimal Conceptual Design of Two-Stage Reusable Rocket Vehicles Including Trajectory Optimization , 2004 .

[5]  Eric N. Johnson,et al.  On-Line Trajectory Optimization for Autonomous Air Vehicles , 2003 .

[6]  Eric N. Johnson,et al.  REUSABLE LAUNCH VEHICLE ADAPTIVE GUIDANCE AND CONTROL USING NEURAL NETWORKS , 2001 .

[7]  Xinghong Jiang,et al.  General method for internal ballistic analysis of complex propellant grain , 1997 .

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

[9]  Walter E. Hammond,et al.  Design Methodologies for Space Transportation Systems , 2001 .

[10]  Peter H. Zipfel,et al.  Modeling and Simulation of Aerospace Vehicle Dynamics , 2001 .

[11]  Angelo Miele,et al.  Design feasibility via ascent optimality for next-generation spacecraft 1 1 Paper 1AF-98-A.1.04 pres , 1999 .

[12]  Ernst Messerschmid,et al.  Multidisciplinary design tool for system and mission optimization of launch vehicles , 1996 .

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

[14]  Jaroslaw Sobieszczanski-Sobieski,et al.  Multidisciplinary aerospace design optimization - Survey of recent developments , 1996 .

[15]  S. N. Balakrishnan,et al.  HYPERSONIC VEHICLE TRAJECTORY OPTIMIZATION AND CONTROL , 1997 .

[16]  Dieter M. Wolf TRANSYS: Space transportation system preliminary design software , 1994 .