Initial three-dimensional low-thrust trajectory design
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[1] Anastassios E. Petropoulos,et al. Shape-Based Algorithm for Automated Design of Low-Thrust, Gravity-Assist Trajectories , 2004 .
[2] Gang Zhang,et al. Simple Shaping Approximation for Low-Thrust Trajectories Between Coplanar Elliptical Orbits , 2015 .
[3] R. V. Dooren,et al. A Chebyshev technique for solving nonlinear optimal control problems , 1988 .
[4] Hexi Baoyin,et al. Low-cost transfer between asteroids with distant orbits using multiple gravity assists , 2015 .
[5] Ehsan Taheri,et al. Non-linear solution to the maximum height orbit transfer guidance problem , 2012 .
[6] Alessandro Antonio Quarta,et al. Escape from Elliptic Orbit Using Constant Radial Thrust , 2009 .
[7] B. Conway. Spacecraft Trajectory Optimization , 2014 .
[8] Frederick W. Boltz. Orbital motion under continuous radial thrust , 1991 .
[9] Hsue-shen Tsien,et al. Take-Off from Satellite Orbit , 1953 .
[10] Howard D. Curtis,et al. Orbital Mechanics for Engineering Students , 2005 .
[11] Daniel Novak,et al. Improved Shaping Approach to the Preliminary Design of Low-Thrust Trajectories , 2011 .
[12] Frederick W. Boltz,et al. ORBITAL MOTION UNDER CONTINUOUS TANGENTIAL THRUST , 1992 .
[13] K. J. Schwenzfeger. Asymptotic solution to the tangential low thrust energy increase trajectory , 1973 .
[14] Massimiliano Vasile,et al. On the optimality of a shape-based approach based on pseudo-equinoctial elements , 2006 .
[15] Massimiliano Vasile,et al. Preliminary Design of Low-Thrust Multiple Gravity-Assist Trajectories , 2006 .
[16] R. Epenoy,et al. New smoothing techniques for solving bang–bang optimal control problems—numerical results and statistical interpretation , 2002 .
[17] O. Abdelkhalik,et al. Fast Initial Trajectory Design for Low-Thrust Restricted-Three-Body Problems , 2015 .
[18] A. Quarta,et al. Multi-revolution transfer for heliocentric missions with solar electric propulsion , 2015 .
[19] Jean Albert Kechichian,et al. Reformulation of Edelbaum' s Low-Thrust Transfer Problem Using Optimal Control Theory , 1997 .
[20] J. Betts. Survey of Numerical Methods for Trajectory Optimization , 1998 .
[21] Massimiliano Vasile,et al. Direct transcription of low-thrust trajectories with finite trajectory elements , 2012 .
[22] Ehsan Taheri,et al. Aircraft Optimal Terrain/Threat-Based Trajectory Planning and Control , 2014 .
[23] Xibin Cao,et al. Modified inverse-polynomial shaping approach with thrust and radius constraints , 2015 .
[24] D. Izzo,et al. Time-optimal trajectories to circumsolar space using solar electric propulsion , 2013 .
[25] Michael A. Saunders,et al. SNOPT: An SQP Algorithm for Large-Scale Constrained Optimization , 2002, SIAM J. Optim..
[26] Ossama Abdelkhalik,et al. Approximate On-Off Low-Thrust Space Trajectories Using Fourier Series , 2012 .
[27] Xu Bo,et al. Optimal strategy for low-thrust spiral trajectories using Lyapunov-based guidance , 2015 .
[28] Bradley J. Wall,et al. Shape-Based Approach to Low-Thrust Rendezvous Trajectory Design , 2009 .
[29] D. J. Benney. Escape From a Circular Orbit Using Tangential Thrust , 1958 .
[30] R. Noomen,et al. Hodographic-Shaping Method for Low-Thrust Interplanetary Trajectory Design , 2015 .
[31] Anil V. Rao,et al. Algorithm 902: GPOPS, A MATLAB software for solving multiple-phase optimal control problems using the gauss pseudospectral method , 2010, TOMS.
[32] Ossama Abdelkhalik,et al. Shape-Based Approximation of Constrained Low-Thrust Space Trajectories Using Fourier Series , 2012 .