Optimization and Guidance Scheme of Constant Low-Thrust Transfers to Geostationary Orbit
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[1] Steven R. Oleson,et al. Direct Approach for Computing Near-Optimal Low-Thrust Earth-Orbit Transfers , 1998 .
[2] Bruce A. Conway,et al. Particle Swarm Optimization Applied to Space Trajectories , 2010 .
[3] Yang Gao,et al. Near-Optimal Very Low-Thrust Earth-Orbit Transfers and Guidance Schemes , 2007 .
[4] P. Gurfil. Nonlinear feedback control of low-thrust orbital transfer in a central gravitational field , 2007 .
[5] Chao Han,et al. Formation design in elliptical orbit using relative orbit elements , 2012 .
[6] Jean-Baptiste Caillau,et al. 3D Geosynchronous Transfer of a Satellite: Continuation on the Thrust , 2003 .
[7] D. Spencer,et al. Optimal Continuous Thrust Orbit Transfer Using Evolutionary Algorithms , 2004 .
[8] J. Betts. Survey of Numerical Methods for Trajectory Optimization , 1998 .
[9] David H. Lehman,et al. Results from the Deep Space 1 technology validation mission , 2000 .
[10] Craig A. Kluever,et al. Trajectory-Tracking Guidance Law for Low-Thrust Earth-Orbit Transfers , 2000 .
[11] Craig A. Kluever,et al. Simple Guidance Scheme for Low-Thrust Orbit Transfers , 1998 .
[12] Thomas Haberkorn,et al. Low thrust minimum-fuel orbital transfer: a homotopic approach , 2004 .
[13] Jean Albert Kechichian. OPTIMAL LOW-THRUST RENDEZVOUS USING EQUINOCTIAL ORBIT ELEMENTS , 1996 .
[14] Giuseppe D. Racca,et al. SMART 1: The first small mission for advanced research in technology , 1999 .
[15] L. Biegler,et al. Real Time Optimal Guidance of Low‐Thrust Spacecraft: An Application of Nonlinear Model Predictive Control , 2005, Annals of the New York Academy of Sciences.
[16] Chao Han,et al. Dynamics and Control of Satellite Formation Flying Based on Relative Orbit Elements , 2008 .