## 留言板

 引用本文: 李世鹏, 梁欣欣, 荣晶晶, 等 . 固体运载器飞行动力学逆问题分类[J]. 北京航空航天大学学报, 2014, 40(8): 1017-1021.
Li Shipeng, Liang Xinxin, Rong Jingjing, et al. Classification of inverse problem of solid launch vehicle flight dynamics[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(8): 1017-1021. doi: 10.13700/j.bh.1001-5965.2013.0516(in Chinese)
 Citation: Li Shipeng, Liang Xinxin, Rong Jingjing, et al. Classification of inverse problem of solid launch vehicle flight dynamics[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(8): 1017-1021. (in Chinese)

## 固体运载器飞行动力学逆问题分类

##### doi: 10.13700/j.bh.1001-5965.2013.0516

###### 作者简介:李世鹏（1978-），男，河北石家庄人，高级工程师，flitan@163.com.
• 中图分类号: V412.1

## Classification of inverse problem of solid launch vehicle flight dynamics

• 摘要: 为了降低问题分析及求解难度，对固体运载器出现的飞行动力学逆问题进行了分类研究.通过归纳逆问题解的特点，将其分为3类，并给出了每类问题的统一提法.进一步提出了逆问题的解析求解和优化求解2种基本解法.解析解法通常求解较快，但精度不高.优化求解可以得到较为精确的解，但通常耗时.针对每类动力学逆问题选取有代表性的典型工程问题，即主发动机需用推力设计、合外力辨识和误差分离问题，分别进行了分析并得到了求解结果.典型工程问题的分析和计算结果表明了分类的合理性.

•  [1] Rohlf D, Schmidt S,Irving J.Stability and control analysis for an unmanned aircraft configuration using system-identification techniques[J].Journal of Aircraft,2012,49(6):1597-1609 [2] Hamel P G, Jategaonkar R V.Evolution of flight vehicle system identification[J].Journal of Aircraft,1996,33(1):9-28 [3] 杨超. 直升机飞行动力学逆问题研究综述[J].飞行力学,2000,18(2):5-8 Yang Chao.Summary about inverse problem of helicopter flight dynamics[J].Flight Dynamics,2000,18(2):5-8(in Chinese) [4] Malone J B, Vadyak J,Sankar L N.Inverse aerodynamic design method for aircraft components[J].Journal of Aircraft,1987, 24(1): 8-9 [5] Ata A A. Inverse dynamic analysis and trajetory planning for flexible manipulator[J].Inverse Problems in Science and Engineering,2010,18(4):549-566 [6] Mira-Cristiana A. The energy-free equations of the 3D inverse problem of dynamics[J].Inverse Problems in Science and Engineering,2005,13(5): 545-558 [7] 杨超,熊良玉,张晓谷. 直升机机动飞行逆仿真研究[J].北 京航空航天大学学报,2000,26(6):697-700 Yang Chao,Xiong Liangyu,Zhang Xiaogu.Inverse simulation for helicopter maneuvering flight[J].Journal of Beijing University of Aeronautics and Astronautics,2000,26(6):697-700(in Chinese) [8] 梅凤翔. 动力学逆问题[J].北京:国防工业出版社,2009 Mei Fengxiang.Inverse problem of dynamics[M].Beijing:National Defence Industrial Press,2009(in Chinese) [9] 龙乐豪. 总体设计(I)[M].北京:中国宇航出版社,1993 Long Lehao.System design(I)[M].Beijing:China Astronautic Publishing House,1993(in Chinese) [10] 贾沛然,陈克俊,何力.远程火箭弹道学[M].长沙:国防科技大学出版社,1993 Jia Peiran,Chen Kejun,He Li.Long-range rocket ballistics[M].Changsha:National University of Defence Technology Press,1993(in Chinese) [11] 梁欣欣,辛万青, 张耐民,等.基于组合算法的多级固体运载火箭运载能力优化[J].导弹与航天运载技术, 2011(5): 6- 10 Liang Xinin,Xin Wanqing,Zhang Naimin,et al.Launch capability optimization for multi-stage solid launch vehicle using a hybrid optimization method[J]. Missiles and Space Vehicles,2011(5):6-10(in Chinese) [12] 洪蓓,梁欣欣,辛万青. 固体运载火箭多约束弹道优化[J]. 导弹与航天运载技术, 2012(3):1-5 Hong Bei,Liang Xinxin,Xin Wanqing.Multi-constraint trajectory optimization for solid launch vehicle[J].Missiles and Space Vehicles,2012(3):1-5(in Chinese) [13] 李瑜,杨志红,崔乃刚. 助推-滑翔导弹弹道优化研究[J].宇航学报,2008,29(1):66-71 Li Yu,Yang Zhihong,Cui Naigang.A study of optimal trajectory for boost-glide missile[J].Journal of Astronautics,2008, 29(1): 66-71(in Chinese) [14] 刘欣,杨涛,张青斌. 助推-滑翔导弹弹道优化与总体参数分析[J].弹道学报,2012,24(3):43-48 Liu Xin,Yang Tao,Zhang Qingbin.Trajectory optimization and parameter analysis for boost-glide missile[J].Journal of Ballistics,2012,24(3):43-48(in Chinese) [15] 龙乐豪. 总体设计(Ⅱ)[M].北京:中国宇航出版社,1993 Long Lehao.System design(Ⅱ)[M].Beijing:China Astronautic Publishing House,1993(in Chinese)

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##### 出版历程
• 收稿日期:  2013-09-22
• 刊出日期:  2014-08-20

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