[1]刘 伟,李欣益,管再升,等.地空导弹通用弹道仿真系统设计与实现[J].弹箭与制导学报,2018,38(02):35-38.[doi:10.15892/j.cnki.djzdxb.2018.02.008]
 LIU Wei,LI Xinyi,GUAN Zaisheng,et al.Design and Implementation of General-aurpose Trajectory Simulation System for Ground-to-air Missile[J].,2018,38(02):35-38.[doi:10.15892/j.cnki.djzdxb.2018.02.008]
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地空导弹通用弹道仿真系统设计与实现

参考文献/References:

[1] BRAUER G L, COMIEK D E, STEVENSON R. Capabilities and applications of the program to optimize simulated trajectories(POST): Program summary document: NASA-CR-2770 [R].[S.l.:s.n.], 1977.
[2] HARGRAVES C R, PARIS SW, VLASES W G. OTIS past: present and future: AIAA PAPER 92-4530[R]. [S.l.s.n.], 1992.
[3] 唐明亮. 飞行器弹道仿真通用软件设计 [D]. 西安: 西北工业大学, 2006.
[4] 鲁中华. 导弹通用弹道模型建立及仿真验证 [D]. 长沙: 国防科技大学, 2009.
[5] 龚春林, 谷良贤. 导弹总体方案设计软件系统设计与实现 [J]. 计算机仿真, 2012, 29(6): 71-74.
[6] 赵军民, 何亚娟. 基于MATLAB/Simulink的弹道仿真模块化设计 [J].弹箭与制导学报, 2007, 27(1): 147-
149.
[7] 王仲铎. 防空导弹可视化弹道仿真技术研究 [D]. 南京: 南京理工大学, 2013.
[8] 洪蕾. 导弹飞行仿真可视化系统研究与实现 [J]. 弹箭与制导学报, 2007, 27(3): 91-94.

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备注/Memo

收稿日期:2017-05-19 第一作者简介:刘伟(1984-),男,山东滨州人,高级工程师,硕士研究生,研究方向:防空导弹弹道设计、总体设计。

更新日期/Last Update:

2018-02-11