[1] |
Conway B A. Spacecraft trajectory optimization[M].UK:Cambridge University Press,2010.
|
[2] |
Kemble S. Interplanetary mission analysis and design[M].Netherland:Springer Science & Business Media,2006.
|
[3] |
Bryson A E,Ho Y. Applied optimal control:optimization,estimation and control[M]. Boca Raton:CRC Press,1975.
|
[4] |
Gill P E,Murray W,Saunders M A,et al. User's guide for NPSOL(Version 4.0):a FORTRAN package for nonlinear programming[M]. USA:Department of Operations Research,Stanford University,1986.
|
[5] |
Gill P E,Murray W,Saunders M A. SNOPT:an SQP algorithm for large-scale constrained optimization[J]. SIAM Review,2002,47:99-131.
|
[6] |
Gill P E,Murray W,Saunders M A. User's guide for SNOPT version 7:software for large scale nonlinear programming[M]. Research Gate,2008.
|
[7] |
Springer B. KNITRO:an integrated package for nonlinear optimization[J]. Large Scale Nonlinear Optimization,2010,83:35-59.
|
[8] |
Betts J T. Survey of numerical methods for trajectory optimization[J]. Journal of Guidance,Control,and Dynamics,1998,21(2):193-207.
|
[9] |
Rao A V. A survey of numerical methods for optimal control[J]. Advances in the Astronautical Sciences,2009,135(1):497-528.
|
[10] |
高扬. 电火箭星际航行:技术进展、轨道设计与综合优化[J]. 力学学报,2011,43(6):991-1019.Gao Y. Interplanetary travel with electric propulsion:technological progress,trajectory design,and comprehensive optimization[J]. Chinese Journal of Theoretical and Applied Mechanics,2011,43(6):991-1019.
|
[11] |
李俊峰,蒋方华. 连续小推力航天器的深空探测轨道优化方法综述[J]. 力学与实践,2011,33(3):1-6.Li J,Jiang F. Survey of low-thrust trajectory optimization methods for deep space exploration[J]. Mechanics in Engineering,2011,33(3):1-6.
|
[12] |
Pontryagin L S,Boltyansky V G,Gamkrelidze R V,et al. The mathematical theory of optimal processes[M]. New York:Interscience Publishers,1962.
|
[13] |
Bartholomew-Biggs M C,Dixon L C W,Hersom S E,et al. From high thrust to low thrust:an application of advanced optimisation methods to mission analysis[J]. ESA J.,1983,11:61-73.
|
[14] |
Dixon L C W,Hersom S E,Maany Z A. Low thrust orbit optimisation for interplanetary missions[R]. The Hatfield Polytechnic:Technical Report 137,Numerical Optimisation Centre,1983.
|
[15] |
Dixon L C W,Maany Z A. To bus and back[C]//ESA Proceedings of the Second International Symposium on Spacecraft Flight Dynamics. Darmstadt,Germany:ESA,1986.
|
[16] |
Bartholomew-Biggs M C,Dixon L C W,Hersom S E,et al. The solution of some difficult problems in low-thrust interplanetary trajectory optimization[J]. Optimal Control Applications and Methods,1988,9:229-251.
|
[17] |
Oberle H J,Taubert K. Existence and multiple solutions of the minimum-fuel orbit transfer problem[J]. Journal of Optimization Theory and Applications,1997,95(2):243-262.
|
[18] |
Fowler W T,O'Neill P M. Relationship between coast arc length and switching function value during optimization[J]. Journal of Spacecraft and Rockets,1976,3(7):445-446.
|
[19] |
Chuang C H,Goodson T,Hanson J. Fuel-optimal,low-and medium-thrust orbit transfers in large numbers of burns[C]//AIAA 94-3650,Guidance,Navigation,and Control Conference.USA:AIAA,1994.
|
[20] |
Chuang J C H,Goodson T D,Hanson J. Multiple-burn families of optimal low-and medium-thrust orbit transfers[J]. Journal of Spacecraft and Rockets,1999,36(6):866-874.
|
[21] |
Redding D C. Highly efficient,very low-thrust transfer to geosynchronous orbit-Exact and approximate solutions[J]. Journal of Guidance,Control,and Dynamics,1984,7(2):141-147.
|
[22] |
Redding D,Breakwell J V. Optimal low-thrust transfers to synchronous orbit[J]. Journal of Guidance,Control,and Dynamics,1984,7(2):148-155.
|
[23] |
Gao,Y. Near-optimal very low-thrust Earth-orbit transfers and guidance schemes[J]. Journal of Guidance,Control,and Dynamics,2007,30(2):529-539.
|
[24] |
Zuiani F,Vasile M. Preliminary design of debris removal missions by means of simplified models for low-thrust,many-revolution transfers[J]. International Journal of Aerospace Engineering,2012.
|
[25] |
Goodson T,Chuang J C H,Hanson J,et al. Optimal finite thrust orbit transfers with large numbers of burns[J]. Journal of Guidance,Control,and Dynamics,1999,22(1):139-148.
|
[26] |
Bai X,Turner J D,Junkins J L. A robust homotopy method for equality constrained nonlinear optimization[C]//AIAA 2008-5845,12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. Columbia:AIAA,2008.
|
[27] |
Bai X,Turner J D,Junkins J L. Optimal thrust design of a mission to apophis based on a homotopy method[C]//AAS/AIAA Spaceflight Mechanics Meeting. Georgia:AIAA,2009.
|
[28] |
Bai X,Turner J D,Junkins J L. Bang-Bang control design by combing pseudospectral method with a novel homotopy algorithm[C]//AIAA Guidance,Navigation,and Control Conference and Control Conference.[S.l.]:AIAA,2009.
|
[29] |
Shan J,Ren Y. Low-thrust trajectory design with constrained particle swarm optimization[J]. Aerospace Science and Technology,2014,36:114-124.
|
[30] |
Darby C L,Hager W W,Rao A V. Direct trajectory optimization using a variable low-order adaptive pseudospectral method[J]. Journal of Spacecraft and Rockets,2011,48(3):433-445.
|
[31] |
Zondervan K P. Optimal low thrust,three burn orbit transfers with large plane changes[D]. California:California Institute of Technology,1983.
|
[32] |
Zondervan K P,Wood L J,Caughey T K. Optimal low-thrust,three-burn orbit transfers with large plane changes[J]. Journal of the Astronautical Sciences,1984,32(3):407-427.
|
[33] |
Ilgen M R. Hybrid method for computing optimal low thrust OTV trajectories[J]. Advances in the Astronautical Sciences,1994,87(2):941-958.
|
[34] |
Kluever C A,Pierson B L. Optimal Low-Thrust Three-Dimensional Earth-Moon trajectories[J]. Journal of Guidance,Control,and Dynamics,1995,18(4):830-837.
|
[35] |
Gao Y,Kluever C A. Low-thrust interplanetary orbit transfers using hybrid trajectory optimization method with multiple shooting[C]//AIAA/AAS Astrodynamics Specialist Conference and Exhibit,Providence. Rhode Island:AIAA,2004.
|
[36] |
Bertrand R.,Epenoy R. New smoothing techniques for solving bang-bang optimal control problems:numerical results and statistical interpretation[J]. Optimal Control Applications and Methods,2002,23(4):171-197.
|
[37] |
Haberkorn T,Martinon P,Gergaud J. Low thrust minimum-fuel orbital transfer:a homotopic approach[J]. Journal of Guidance,Control,and Dynamics,2004,27(6):1046-1060.
|
[38] |
Gergaud,J,Haberkorn T. Homotopy method for minimum consumption orbit transfer problem[J]. ESAIM:Control,Optimization,and Calculus of Variations,2006,12(2):294-310.
|
[39] |
Gergaud J,Haberkorn T. Orbital transfer:some links between the low-thrust and the impulse cases[J]. Acta Astronautica,2007,60(8-9):649-657.
|
[40] |
Martinon P,Gergaud J. Using switching detection and variational equations for the shooting method[J]. Optimal Control Applications and Methods,2007,28(2):95-116.
|
[41] |
Petukhov V G. Optimization of interplanetary trajectories for spacecraft with ideally regulated engines using the continuation method[J]. Cosmic Research,2008,46(3):219-232.
|
[42] |
Petukhov V G. Method of continuation for optimization of inth Capabilities of Indirect Methods for Impulsive Transfers[J]. The Journal of the Astronautical Sciences,2015,62(3):212-232.
|
[43] |
Shen H X,Casalino L,Li H Y. Adjoints estimation methods for impulsive Moon-to-Earth trajectories in the restricted three-body problem[J]. Optimal Control Applications and Methods,2015,36(4):463-474.
|
[44] |
Shen H X,Casalino L. Indirect optimization of three-dimensional multiple-impulse Moon-to-Earth transfers[J]. The Journal of the Astronautical Sciences,2014,61(3):255-274.teroid tour missions[J]. Journal of Guidance,Control,and Dynamics,2011,34(6):1709-1720.
|
[45] |
Guo T,Jiang F,Baoyin H,et al. Fuel optimal low thrust rendezvous with outer planets via gravity assist[J]. Science China:Physics,Mechanics and Astronomy,2011,54(4):756-769.
|
[46] |
Guo T,Jiang F,Li J. Homotopic approach and pseudospectral method applied jointly to low thrust trajectory optimization[J]. Acta Astronautica,2012,71:38-50.
|
[47] |
Jiang F,Baoyin H,Li J. Practical Techniques for low-thrust trajectory optimization with homotopic approach[J]. Journal of Guidance,Control,and Dynamics,2012,35(1):245-258.
|
[48] |
Li J,Xi X-N. Fuel-optimal low-thrust reconfiguration of formation-flying satellites via homotopic approach[J]. Journal of Guidance,Control,and Dynamics,2012,35(6):1709-1717.
|
[49] |
Tarzi Z,Speyer J,Wirz R. Fuel optimum low-thrust elliptic transfer using numerical averaging[J]. Acta Astronautica,2013,86:95-118.
|
[50] |
Zhang P,Li J,Baoyin H,Tang G. A low-thrust transfer between the Earth-Moon and Sun-Earth systems based on invariant monifolds[J]. Acta Astronautica,2013,91:77-88.
|
[51] |
Chen Y,Baoyin H,Li J. Accessibility of main-belt asteroids via gravity assists[J]. Journal of Guidance,Control,and Dynamics,2014,37(2):623-632.
|
[52] |
Zhang P,Li J,Gong S. Fuel-optimal trajectory design using solar electric propulsion under power constraints and performance degradation[J]. Science China Physics,Mechanics & Astronomy,2014,57(6):1090-1097.
|
[53] |
Zhang C,Topputo F,Bernelli-Zazzera F,et al. Low-thrust minimum-fuel optimization in the circular restricted three-body problem[J]. Journal of Guidance,Control,and Dynamics,2015,38(8):1501-1510.
|
[54] |
张晨,赵育善. 混合推进最省燃料轨道设计方法[J]. 宇航学报,2015,36(8):869-876.Zhang C,Zhao Y. A method for hybrid propulsion minimum fuel trajectory optimization[J]. Journal of Astronautics,2015,36(8):869-876.
|
[55] |
陆毅,李济生,李恒年,等. 基于星历匹配法的载人小行星探测轨迹优化问题求解[J]. 力学与实践,2014,36(2):172-179.Lu Y,Li J,Li H,et al. Problem solving of the manned asteroids exploration trajectory optimization based on ephemeris matching method[J]. Mechanics in Engineering,2014,36(2):172-179.
|
[56] |
黄岸毅,车征,李恒年,等. 有限推力多小行星探测轨迹优化[J]. 力学与实践,2015,37(1):49-55.Huang A,Che Z,Li H,et al. Low-thrust trajectory optimization for multi-asteroid exploration[J]. Mechanics in Engineering,2015,37(1):49-55.
|
[57] |
朱小龙,刘迎春,高扬. 航天器最优受控绕飞轨迹推力幅值延拓设计方法[J]. 力学学报,2014,46(5):756-769.Zhu X,Liu Y,Gao Y. Thrust-amplitude continuation design approach for solving spacecraft optimal controlled fly-around trajectory[J]. Chinese Journal of Theoretical and Applied Mechanics,2014,46(5):756-769.
|
[58] |
朱小龙,马剑,刘强,等. 月面远程运输飞行轨迹优化设计[J]. 载人航天,2015,21(1):75-82.Zhu X,Ma J,Liu Q,Gao Y. Optimization design of long-range transport flight trajectories on lunar surface[J]. Manned Spaceflight,2015,21(1):75-82.
|
[59] |
Battin,R.H. An introduction to the mathematics and methods of astrodynamics[M].[S.l.]:AIAA Education Series,1987.
|
[60] |
朱政帆,甘庆波. 第七届全国空间轨道设计竞赛乙组解法[J]. 力学与实践,2016,38(5):596-602.Zhu Z,Gan Q. 7thNational space trajectory design competition:results of problem B[J]. Mechanics in Engineering,2016,38(5):596-602.
|
[61] |
孟雅哲. 航天器燃耗最优轨道直接/间接混合法延拓求解[J]. 航空学报,2017,38(1):259-280.Meng Y. Minimum-fuel spacecraft transfer trajectories solved by direct/indirect hybrid method with continuation[J]. Acta Aeronautica et Astronautica Sinica,2017,38(1):259-280.
|
[62] |
Zhu Z,Gao Y,Yang X,et al. Solving fuel-optimal low-thrust orbital transfers with bang-bang control using a novel continuation technique[J]. Acta Astronautica,accepted.
|
[63] |
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