一种超音速火箭靶弹程序角优化方法研究

doi:10.3969/j.issn.1000-1093.2015.04.011

兵工学报 ›› 2015, Vol. 36 ›› Issue (4): 644-652.doi: 10.3969/j.issn.1000-1093.2015.04.011

一种超音速火箭靶弹程序角优化方法研究

沈冠军¹, 冯顺山², 曹红松¹

(1.中北大学机电工程学院，山西太原 030051; 2.北京理工大学爆炸科学与技术国家重点实验室，北京 100081)

收稿日期:2014-05-06 修回日期:2014-05-06 上线日期:2015-06-02
作者简介:沈冠军(1987—)，男，博士研究生
基金资助:
兵器“十二五”预先研究支撑基金项目（62201070503）

Research on a Program Angle Optimization Method for Supersonic Rocket Target

SHEN Guan-jun¹, FENG Shun-shan², CAO Hong-song¹

(1.School of Mechatronics Engineering, North University of China, Taiyuan 030051, Shanxi, China;2.State Key Laboratory of Explosion Science and Technology, Beijing Institute of Technology, Beijing 100081, China)

Received:2014-05-06 Revised:2014-05-06 Online:2015-06-02

摘要/Abstract

摘要： 针对方案制导超音速火箭靶弹平飞段供靶性能优化问题，提出了一种俯仰程序角优化方法。考虑靶弹弹道始末端点约束及平飞段性能约束，在火箭靶弹纵向飞行平面内建立起俯仰程序角优化设计模型。基于Gauss伪谱法将飞行过程约束转化成对俯仰程序角的约束，将最优控制问题转换为对俯仰程序角的非线性规划问题；利用序列二次规划算法求解。仿真结果表明，该方法能够快速获取最优俯仰程序角，并且具有良好的鲁棒性，为实际工程设计提供参考。

关键词: 兵器科学与技术, 超音速靶弹, 平飞弹道, 程序角优化, Gauss伪谱法

Abstract: An optimization method of pitch program angle is proposed for the optimization problems of level flight trajectory of supersonic rocket target. Considering the initiation and impact point of rocket target and the level flight state constraints, the pitch program angle optimization model is built on the longitudinal flight plane of rocket target. The Process constraints are transformed to the pitch program angle constraints, and the optimal control problems are translated to the nonlinear programming problems based on Gauss pseudo spectral method. And then the nonlinear programming problems are solved by sequential quadratic programming method. Simulation results show that this proposed method can quickly obtain the optimal program pitch angle, and has good robustness.

Key words: ordnance science and technology, supersonic rocket target, level flight trajectory, program angle optimization, Gauss pseudo spectral method

中图分类号:

TJ013.2

沈冠军, 冯顺山, 曹红松. 一种超音速火箭靶弹程序角优化方法研究[J]. 兵工学报, 2015, 36(4): 644-652.

SHEN Guan-jun, FENG Shun-shan, CAO Hong-song. Research on a Program Angle Optimization Method for Supersonic Rocket Target[J]. Acta Armamentarii, 2015, 36(4): 644-652.

参考文献

［1］张邦楚, 韩子鹏, 范雁飞. 巡航导弹模拟靶平飞弹道设计[J].弹道学报, 2003, 15(2): 28-33.
ZHANG Bang-chu, HAN Zi-peng, FAN Yan-fei. Design of the level trajectory of cruise missile simulated target [J]. Journal of Ballistics, 2003, 15(2):28-33. (in Chinese)
[2] 李晓斌, 王永杰, 孙晓峰. 简易控制火箭靶弹总体设计[J]. 弹道学报, 2010, 22(1): 41-44.
LI Xiao-bin, WANG Yong-jie, SUN Xiao-feng.System design of simple control rocket target[J]. Journal of Ballistics, 2010, 22(1): 41-44. (in Chinese)
[3] 霍鹏飞, 施坤林, 苑伟政. 基于极大值原理的弹道修正引信弹道优化控制研究[J]. 兵工学报, 2007, 27(3): 301-304.
HUO Peng-fei, SHI Kun-lin, YUAN Wei-zheng. Research on trajectory controlled optimization for trajectory correction fuze using maximum principle[J]. Acta Armamentarii, 2007, 27(3): 301-304. (in Chinese)
[4] 李永远, 姜毅, 高伟涛, 等. 间接法求解具有最大横程的再入轨迹[J]. 北京理工大学学报, 2013, 33(7): 665-668.
LI Yong-yuan, JIANG Yi, GAO Wei-tao, et al. Indirect method for solving the reentry trajectory with maximum cross range[J]. Transactions of Beijing Institute of Technology, 2013, 33(7):665-668. (in Chinese)
[5] 李柯, 聂万胜, 冯必鸣. 助推-滑翔飞行器规避能力研究[J]. 飞行力学, 2013, 31(2): 148-156.
LI Ke, NIE Wan-sheng, FENG Bi-ming. Research on elusion capability of boost-glide vehicle[J]. Flight Dynamics, 2013, 31(2): 148-156. (in Chinese)
[6] 水尊师, 周军, 葛致磊. 基于高斯伪谱方法的再入飞行器预测校正制导方法研究[J]. 宇航学报, 2011, 32(6): 1249-1254.
SHUI Zun-shi, ZHOU Jun, GE Zhi-lei. On-line predictor-corrector reentry guidance law based on Gauss pseudospectral method[J]. Journal of Astronautics, 2011, 32(6): 1249-1254. (in Chinese)
[7] Huntington G T. Advancement and analysis of a Gauss pseudospectral transcription for optimal control problems[D]. MA: Massachusetts Institute of Technology, 2007: 23-49.
[8] 林献武. 高空环境下弹箭的弹道特性研究[D].南京: 南京理工大学, 2009: 9-13.
LIN Xian-wu. A research on the ballistic characteristics of projectile flying at high altitude environment[D].Nanjing: Nanjing University of Science and Technology, 2009: 9-13. (in Chinese)
[9] Garg D, Hager W W, Rao A V. Pseudospectral methods for solving infinite-horizon optimal control problems[J].Automatica, 2011, 47(4): 829-837.
[10] Maleki M, Hashim I. Adaptive pseudospectral methods for solving constrained linear and nonlinear time-delay optimal control problems [J].Journal of the Franklin Institute, 2014, 351(2): 811-839.
[11] Rao A V, Clarke K A. Performance optimization of a maneuvering re-entry vehicle using a legendre pseudospectral method[C]∥2002 AIAA Atmospheric Flight Mechanics Conference. Monterey, US: American Institute of Aeronautics and Astronautics, 2002.
[12] Rao A V, Benson D A, Darby C. Algorithm 902: GPOPS, A MATLAB software for solving multiple-phase optimal control problems using the gauss pseudospectral method[J].ACM Transactions on Mathematical Software, 2010, 37(2): 1-39.
[13] Garg D, Rao A V, Hager W W. Gauss pseudospectral method for solving infinite-horizon optimal control problems[C]∥AIAA Guidance, Navigation, and Control Conference.Toronto, Ontario, Canada Toronto: American Institute of Aeronautics and Astronautics, 2010: 1-9.
[14] 郑总准, 吴浩, 王永骥. 基于序列二次规划算法的再入轨迹优化研究[J]. 航天控制, 2009, 27(6): 8-13.
ZHENG Zong-zhun, WU Hao, WANG Yong-ji.Reentry trajectory optimization using sequential quadratic programming[J]. Aerospace Control, 2009, 27(6): 8-13. (in Chinese)

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一种超音速火箭靶弹程序角优化方法研究

Research on a Program Angle Optimization Method for Supersonic Rocket Target

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