RAPID SPACE TRAJECTORY GENERATION USING A FOURIER SERIES SHAPE-BASED APPROACH
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[1] J. Breakwell,et al. OPTIMUM GUIDANCE FOR A LOW THRUST INTERPLANETARY VEHICLE , 1965 .
[2] David H. Lehman,et al. Results from the Deep Space 1 technology validation mission , 2000 .
[3] Bradley J. Wall,et al. Shape-Based Approach to Low-Thrust Rendezvous Trajectory Design , 2009 .
[4] 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.
[5] Ossama Abdelkhalik,et al. Shape-Based Approximation of Constrained Low-Thrust Space Trajectories Using Fourier Series , 2012 .
[6] R. Battin. An introduction to the mathematics and methods of astrodynamics , 1987 .
[7] Edgar Y. Choueiri,et al. A Critical History of Electric Propulsion: The First 50 Years (1906-1956) , 2004 .
[8] Hyochoong Bang,et al. Optimal Earth-Moon Trajectory Design Using New Initial Costate Estimation Method , 2012 .
[9] Anastassios E. Petropoulos,et al. Shape-Based Algorithm for Automated Design of Low-Thrust, Gravity-Assist Trajectories , 2004 .
[10] B. Conway. Spacecraft Trajectory Optimization , 2014 .
[11] K. J. Schwenzfeger. Asymptotic solution to the tangential low thrust energy increase trajectory , 1973 .
[12] Massimiliano Vasile,et al. Preliminary Design of Low-Thrust Multiple Gravity-Assist Trajectories , 2006 .
[13] D. D. Mueller,et al. Fundamentals of Astrodynamics , 1971 .
[14] Massimiliano Vasile,et al. On the optimality of a shape-based approach based on pseudo-equinoctial elements , 2006 .
[15] M. Martinez-Sanchez,et al. Spacecraft Electric Propulsion—An Overview , 1998 .
[16] Howard D. Curtis,et al. Orbital Mechanics for Engineering Students , 2005 .
[17] Daniel Novak,et al. Improved Shaping Approach to the Preliminary Design of Low-Thrust Trajectories , 2011 .
[18] Oskar von Stryk,et al. Direct and indirect methods for trajectory optimization , 1992, Ann. Oper. Res..
[19] Bruce A. Conway,et al. Discrete approximations to optimal trajectories using direct transcription and nonlinear programming , 1992 .
[20] D. J. Benney. Escape From a Circular Orbit Using Tangential Thrust , 1958 .
[21] R. V. Dooren,et al. A Chebyshev technique for solving nonlinear optimal control problems , 1988 .
[22] K.T. Uesugi. Space engineering spacecraft (MUSES) program in ISAS featuring its latest mission "Hayabusa" , 2003, International Conference on Recent Advances in Space Technologies, 2003. RAST '03. Proceedings of.
[23] Frank M. Perkins. Flight Mechanics of Low-Thrust Spacecraft , 1959 .
[24] A. Petropoulos,et al. A shape -based approach to automated, low-thrust, gravity -assist trajectory design , 2001 .
[25] Victoria Coverstone-Carroll,et al. CONSTANT RADIAL THRUST ACCELERATION REDUX , 1998 .
[26] Ossama Abdelkhalik,et al. Approximate On-Off Low-Thrust Space Trajectories Using Fourier Series , 2012 .
[27] T. Paulino,et al. Analytical representations of low-thrust trajectories , 2008 .
[28] Alessandro Antonio Quarta,et al. Escape from Elliptic Orbit Using Constant Radial Thrust , 2009 .
[29] Daniel J. Scheeres,et al. Trajectory Optimization Using the Reduced Eccentric Anomaly Low-Thrust Coefficients , 2008 .
[30] O. Abdelkhalik,et al. Fast Initial Trajectory Design for Low-Thrust Restricted-Three-Body Problems , 2015 .
[31] H. Hancock. Theory of Maxima and Minima , 1919 .
[32] Bradley J. Wall,et al. Shape-Based Approximation Method for Low-Thrust Trajectory Optimization , 2008 .
[33] Frederick W. Boltz. Orbital motion under continuous radial thrust , 1991 .
[34] Ossama Abdelkhalik,et al. Constraint Low-Thrust Trajectory Planning in Three-Body Dynamic Models: Fourier Series Approach , 2014 .
[35] B. M. Mohan,et al. Orthogonal Functions in Systems and Control , 1995 .
[36] H. S. TSIENI. Take-Off from Satellite Orbit , .
[37] Mohsen Razzaghi,et al. Optimal control of linear time-varying systems via Fourier series , 1990 .
[38] Bion L. Pierson,et al. Three-stage approach to optimal low-thrust Earth-moon trajectories , 1994 .
[39] Frederick W. Boltz,et al. ORBITAL MOTION UNDER CONTINUOUS TANGENTIAL THRUST , 1992 .
[40] Mohsen Razzaghi,et al. Solution of linear two-point boundary value problems via Fourier series and application to optimal control of linear systems , 1989 .
[41] Mohsen Razzaghi,et al. Fourier series direct method for variational problems , 1988 .
[42] R. Broucke,et al. Periodic orbits in the restricted three body problem with earth-moon masses , 1968 .
[43] R. Braun,et al. Survey of Global Optimization Methods for Low-Thrust, Multiple Asteroid Tour Missions , 2007 .
[44] Mohsen Razzaghi,et al. Identification of nonlinear differential equations via Fourier series operational matrix for repeated integration , 1995 .
[45] S. Alfano,et al. Optimal many-revolution orbit transfer , 1984 .
[46] Anil V. Rao,et al. ( Preprint ) AAS 09-334 A SURVEY OF NUMERICAL METHODS FOR OPTIMAL CONTROL , 2009 .
[47] James R. Wertz,et al. Mission geometry; orbit and constellation design and management , 2001 .
[48] Marc D. Rayman,et al. Dawn: A mission in development for exploration of main belt asteroids Vesta and Ceres , 2006 .
[49] Craig A. Kluever,et al. Near-Optimal Low-Thrust Lunar Trajectories , 1996 .
[50] J. Betts. Survey of Numerical Methods for Trajectory Optimization , 1998 .
[51] Angelo Miele,et al. Computation of optimal Mars trajectories via combined chemical/electrical propulsion, part 1: baseline solutions for deep interplanetary space , 2004 .
[52] Jean Albert Kechichian,et al. Reformulation of Edelbaum' s Low-Thrust Transfer Problem Using Optimal Control Theory , 1997 .
[53] Stuart A. Stanton,et al. Optimal Orbital Transfer Using a Legendre Pseudospectral Method , 2003 .
[54] Bion L. Pierson,et al. Optimal Earth-Moon Trajectories Using Nuclear Electric Propulsion , 1997 .
[55] Staffan Persson,et al. SMART-1 mission description and development status , 2002 .
[56] J. Hudson,et al. Reduction of Low-Thrust Continuous Controls for Trajectory Dynamics and Orbital Targeting. , 2009 .