参考文献
[1]张泽旭,崔平远,崔祜涛.行星际高速公路技术[J] .宇航学报,2007,28(1):913.
ZHANG Z X, CUI P Y, CUI G T. Interplanetary superhighway technology[J].Journal of Astronautics, 2007,28(1):9:14.
[2]SEUNGWON L, ANASTASSIOS P, PAUL V. A Lowthrust orbit transfer optimization with refined Qlaw and multiobjective genetic algorithm[C]//AAS/AIAA Astrodynamics Specialists Conference. Washington D.C.:AIAA,2005.
[3]BETTS J T. Survey of numerical methods for trajectory optimization[J].Guidance, Control, and Dynamics, 1998, 21(2):193207.
[4]PETROPOULOS A E.Simple control laws for lowthrust orbit transfers[C]//AAS/AIAA Astrodynamics Specialist Conference. Washington D.C.: AIAA, 2003.
[5]PETROPOULOS A E.Lowthrust orbit transfer using candidate lyapunov functions with a mechanism for coasting[C]//AIAA/AAS Astrodynamics Specialist Conference.Washington D.C.:AIAA, 2004.
[6]RODNEY L,ANDERSON,MARTIN W L.Role of invariant manifolds in lowthrust trajectory design[J] Journal of Guidance Control and Dynamics,2009,32(6): 19211930.
[7]DAVID C F, THOMAS A P. EarthMoon libration point orbit stationkeeping: theory, modeling, and operations[J]. Acta Astronautica,2014,94(1):421433.
[8]ZHOU J,XUE L,ZHOU F Q.Computations of low energy escaping/capturing trajectories in hill’s region via an extended poincaré map[J].Journal of Astronautics, 2007,28(3): 643647.
[9]LEI H L,XU B. Highorder solutions of invariant manifolds associated with libration point orbits in the elliptic restricted threebody system[J].Celestial Mechanics and Dynamical Astronomy,2013,117(4): 349384.
[10]ANASTASSIONS E P. Refinements to the Qlaw for lowthrust orbit transfers[C]// AAS 05162, AAS/AIAA Space Flight Mechanics Conference.Washington D.C.:AIAA, 2005. |