Design and optimization of low-energy transfer orbit to Mars with multi-body environment
暂无分享,去创建一个
Yang Sun | HengNian Li | Yi Lu | Yikang Yang | Hengnian Li | Yi Lu | Jisheng Li | Z. Che | Yuanyuan Yang | Yang Sun | JiSheng Li | Zheng Che | YiKang Yang | Yuan Yang
[1] J. Betts. Very low-thrust trajectory optimization using a direct SQP method , 2000 .
[2] C. A. Kluever,et al. OPTIMAL LOW-THRUST ILNTERPLANETARY TRAJECTORIES BY DIRECT METHOD TECHNIQUES , 1997 .
[3] J. Marsden,et al. Dynamical Systems, the Three-Body Problem and Space Mission Design , 2009 .
[4] Robert D. Falck,et al. A Method of Efficient Inclination Changes for Low-thrust Spacecraft , 2002 .
[5] Howard D. Curtis,et al. Orbital Mechanics for Engineering Students , 2005 .
[6] Ming Xu,et al. Research on the transfers to Halo orbits from the view of invariant manifolds , 2012 .
[7] TieDing Guo,et al. Fuel optimal low thrust rendezvous with outer planets via gravity assist , 2011 .
[8] L. Hiday. Optimal transfers between libration-point orbits in the elliptic restricted three-body problem , 1992 .
[9] J. Betts,et al. MESH REFINEMENT IN DIRECT TRANSCRIPTION METHODS FOR OPTIMAL CONTROL , 1998 .
[10] Martin W. Lo,et al. The InterPlanetary Superhighway and the Origins Program , 2002, Proceedings, IEEE Aerospace Conference.
[11] 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.
[12] Guo-Jin Tang,et al. Planning for space station long-duration orbital mission under multi-constraints , 2013 .
[13] Orbit Transfer via Tube Jumping in Planar Restricted Problems of Four Bodies , 2005 .
[14] Hexi Baoyin,et al. Practical Techniques for Low-Thrust Trajectory Optimization with Homotopic Approach , 2012 .
[15] Hexi Baoyin,et al. Trajectory design for the Moon departure libration point mission in full ephemeris model , 2011 .
[16] Bradley J. Wall,et al. Shape-Based Approximation Method for Low-Thrust Trajectory Optimization , 2008 .
[17] Zhen Yang,et al. Robust optimization of nonlinear impulsive rendezvous with uncertainty , 2014 .
[18] Yang Gao,et al. Near-Optimal Very Low-Thrust Earth-Orbit Transfers and Guidance Schemes , 2007 .
[19] Haibin Shang,et al. Interplanetary transfers employing invariant manifolds and gravity assist between periodic orbits , 2013 .
[20] Theodore N. Edelbaum,et al. Propulsion Requirements for Controllable Satellites , 1961 .
[21] Shane D. Ross,et al. Invariant Manifolds, the Spatial Three-Body Problem and Space Mission Design , 2001 .
[22] W. Hager,et al. An hp‐adaptive pseudospectral method for solving optimal control problems , 2011 .
[23] D. Qiao,et al. Opportunities search of transfer between interplanetary halo orbits in ephemeris model , 2013 .
[24] JiSheng Li,et al. Mathematical prototypes for collocating geostationary satellites , 2013 .
[25] J. Longuski,et al. Low-thrust trajectories for human missions to Ceres , 2012 .
[26] Shane D. Ross,et al. Connecting orbits and invariant manifolds in the spatial restricted three-body problem , 2004 .