[1]杨 靖,毛 瑞,杜凤怀,等.基于高斯伪谱法的制导火箭弹总体优化设计研究[J].弹箭与制导学报,2018,38(5):23-26.[doi:10.15892/j.cnki.djzdxb.2018.05.006]
 YANG Jing,MAO Rui,DU Fenghuai,et al.Study on System Design and Optimization for Guided Rockets Using Gauss Pseudospectral Method[J].,2018,38(5):23-26.[doi:10.15892/j.cnki.djzdxb.2018.05.006]
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基于高斯伪谱法的制导火箭弹总体优化设计研究

参考文献/References:

[1] 杨树兴. 陆军多管火箭武器的发展和思考 [J]. 兵工学报, 2016, 37(7): 1299-1305.
[2] BENSON D. A Gauss pseudo-spectral transcription for optimal control [M]. Cambridge: Massachusetts Institute of Technology, 2005:237-242.
[3] KANG W, BEDROSSIAN N. Pseudospectral optimal control theory makes debut flight, saves NASA $1M in under three hours [J]. SIAM News, 2007,40(7)L1-3.
[4] BEDROSSIAN N, BHATT S, LAMMERS M, et al. Zero-propellant maneuverTM flight results for 180 deg ISS rotation [C]∥NASA. Proceedings of 20th International Symposium on Space Flight Dynamics.Houston:NASA Jonhnson Space Center,2008:1-10.
[5] 杨博, 陈子匀, 温正, 等. 基于高斯伪谱法的化-电混合推进系统转移轨道优化设计 [J]. 中国空间科学技术, 2016, 36(1): 18-25.
[6] 张佩俊, 刘鲁华, 王建华. 基于高斯伪谱法的空天飞机上升段最优轨迹设计 [J]. 空间控制技术与应用, 2017, 43(2): 13-20.

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备注/Memo

收稿日期:2018-01-10 第一作者简介:杨靖(1988-),男,内蒙古杭锦后旗人,博士研究生,研究方向:弹箭总体优化设计。

更新日期/Last Update:

2018-10-25