Optics and Precision Engineering, Volume. 26, Issue 12, 2923(2018)
Fast trajectory-orbit unified design for spacecrafts
[1] [1] LI X G, WANG CH X, WANG W H. Energy management trajectory design of solid launch vehicle based on modified Newton method [J]. Journal of Solid Rocket Technology, 2013, 36(1): 1-5, 16. (in Chinese)
[2] [2] LI ZH H, XIAN Y, LEI G, et al.. Rapid optimization design of ascent rendezvous trajectory for launch vehicles based on hybrid particle swarm algorithm [J]. Journal of Aerospace Power, 2015, 30(12): 3029-3034. (in Chinese)
[3] [3] HU Y, WANG H. Trajectory optimization method of air-launched vehicle based on adaptive genetic algorithm [J]. Journal of North University of China: Natural Science Edition, 2016, 37(2) : 137-141.(in Chinese)
[4] [4] WANG H F, ZHAO J F, WANG W. Research on general trajectory design and simulation for mission level ballistic missile [J]. Computational Simulation, 2016, 33(6) : 64-68, 90. (in Chinese)
[5] [5] NELSON D.Qualitative and quantitative assessment of Optimal Trajectories by Implicit Simulation (OTIS) and Program to Optimize Simulated Trajectories (POST)[Z]. Atlanta: Georgia Institute of Technology, 2001, 4: 24-29.
[6] [6] FANG Q, LIU Y S, WANG X F. Trajectory-orbit unified design for aerospace vehicles [J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(4) : 59-68 .(in Chinese)
[7] [7] LU P, BRUNNER C W, STACHOWIAK S J, et al.. Verification of a fully numerical entry guidance algorithm [J]. Journal of Guidance, Control, and Dynamics, 2016, 40(2): 230-247.
[8] [8] BROYDEN C G. A class of methods for solving nonlinear simultaneous equations [J]. Mathematics of Computation, 1965, 19(92): 577-593.
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WANG Jie-gang, PU Jia-lun, LI Yuan, WANG Ming-ze. Fast trajectory-orbit unified design for spacecrafts[J]. Optics and Precision Engineering, 2018, 26(12): 2923
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Received: Jul. 2, 2018
Accepted: --
Published Online: Jan. 27, 2019
The Author Email: Jie-gang WANG (13901370775@163.com)