| Citation: | ZHU W S，LYU X J，HOU Z Q，et al. Trajectory optimization of air-to-surface missile in full airspace based on combinational optimization algorithm[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（2）：344-352 （in Chinese） doi: 10.13700/j.bh.1001-5965.2021.0252
|
To deal with the problem of trajectory optimization for the air-to-surface missile in full airspace, a combinational optimization algorithm based on a multi-island genetic algorithm (MIGA) and sequential quadratic programming (SQP) was proposed. The advantages of being insensitive to initial values and global convergence of MIGA, and rapid convergence and high precision of SQP were developed. With the surrogate model, the computational cost of trajectory optimization in full airspace was greatly reduced on the premise of ensuring fitting precision. The surrogate model significantly lowered the computing cost of trajectory optimization in full airspace under the assumption of fitting precision. Results show that the combinational optimization algorithm had a rapid convergence speed and could obtain a global high-precision solution; the surrogate model had high fitting precision and could satisfy the requirements of engineering; the optimization results and surrogate model could provide an effective way for the design of guidance law in full airspace.
| [1] |
樊会涛. 空空导弹方案设计原理[M]. 北京: 航空工业出版社, 2013: 67-74.
FAN H T. Air-to-air missile conceptual design[M]. Beijing: Aviation Industry Press, 2013: 67-74(in Chinese).
|
| [2] |
樊会涛, 崔颢, 天光. 空空导弹70年发展综述[J]. 航空兵器, 2016(1): 3-12.
FAN H T, CUI H, TIAN G. A review on the 70-year development of air-to-air missiles[J]. Aero Weaponry, 2016(1): 3-12(in Chinese).
|
| [3] |
向开恒, 李人杰, 陈杨. 基于代理模型的空间飞越发射窗口[J]. 北京航空航天大学学报, 2018, 44(12): 2613-2620.
XIANG K H, LI R J, CHEN Y. Launch window of space fly-by based on surrogate model[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(12): 2613-2620(in Chinese).
|
| [4] |
汤祁忠, 李雄, 叶茂, 等. 基于经典遗传算法的末端多约束弹道优化方法[J]. 战术导弹技术, 2019(4): 1-6.
TANG Q Z, LI X, YE M, et al. Trajectory optimization method with end-piece multiple constraints based on classical genetic algorithm[J]. Tactical Missile Technology, 2019(4): 1-6(in Chinese).
|
| [5] |
李怡昕, 李旭, 刘少波, 等. 高斯伪谱法在变推力导弹弹道优化中的应用[J]. 现代防御技术, 2019, 47(3): 71-77.
LI Y X, LI X, LIU S B, et al. Application of gauss pseudo-spectral method in trajectory optimization of variable trust missile[J]. Modern Defence Technology, 2019, 47(3): 71-77(in Chinese).
|
| [6] |
李伟喆, 陈万春. 双脉冲中程空空导弹弹道优化[J]. 战术导弹技术, 2018(5): 19-24.
LI W Z, CHEN W C. Trajectory optimization of dual-pulse medium range air-to-air missile[J]. Tactical Missile Technology, 2018(5): 19-24(in Chinese).
|
| [7] |
韩聪聪, 何华锋, 杨宗浩. 基于单纯形-遗传算法的导弹主动段优化设计[J]. 电光与控制, 2017, 24(10): 22-26.
HAN C C, HE H F, YANG Z H. Optimization design of missile active phase based on simplex method and GA[J]. Electronics Optics & Control, 2017, 24(10): 22-26(in Chinese).
|
| [8] |
王荣, 张红军, 王贵东, 等. 吸气式空空导弹外形多学科一体化优化设计[J]. 航空学报, 2016, 37(1): 207-215.
WANG R, ZHANG H J, WANG G D, et al. Multidisciplinary integrated design optimization for an airbreathing air-to-air missile shape[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(1): 207-215(in Chinese).
|
| [9] |
黄诘, 张友安, 刘永新. 一种有撞击角和视场角约束的运动目标的偏置比例导引算法[J]. 宇航学报, 2016, 37(2): 195-202.
HUANG J, ZHANG Y A, LIU Y X. A biased proportional guidance algorithm for moving target with impact angle and field-of-view constraints[J]. Journal of Astronautics, 2016, 37(2): 195-202(in Chinese).
|
| [10] |
赵曜, 李璞, 刘娟, 等. 带碰撞角约束的三维有限时间滑模制导律[J]. 北京航空航天大学学报, 2018, 44(2): 273-279.
ZHAO Y, LI P, LIU J, et al. Finite-time sliding mode control based 3D guidance law with impact angle constraints[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(2): 273-279(in Chinese).
|
| [11] |
杨雪榕, 梁加红, 李晓冬. 空空导弹高抛弹道仿真研究[J]. 系统仿真学报, 2010, 22(5): 1261-1265.
YANG X R, LIANG J H, LI X D. Study on parabola-trajectory simulation of air-to-air missile[J]. Journal of System Simulation, 2010, 22(5): 1261-1265(in Chinese).
|
| [12] |
陈韵, 常燕, 苗昊春, 等. 落角约束最优制导律在空地导弹上的应用[J]. 弹箭与制导学报, 2018, 38(5): 141-144.
CHEN Y, CHANG Y, MIAO H C, et al. Optimal guidance law with terminal angular constraint use in air-to-ground missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2018, 38(5): 141-144(in Chinese).
|
| [13] |
ERER K S, TEKIN R. Impact time and angle control based on constrained optimal solutions[J]. Journal of Guidance, Control, and Dynamics, 2016, 39(10): 1-7.
|
| [14] |
史绍琨, 赵久奋, 崇阳, 等. 带落角约束的新型二阶滑模三维制导律[J]. 北京航空航天大学学报, 2019, 45(3): 614-623.
SHI S K, ZHAO J F, CHONG Y, et al. Novel second-order sliding mode control based 3D guidance law with impact angle constraints[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(3): 614-623(in Chinese).
|
| [15] |
魏黎明, 李晓龙, 赵征, 等. 神经网络在吸气式高超声速导弹突防弹道设计上的应用[J]. 空天防御, 2018, 1(2): 14-17.
WEI L M, LI X L, ZHAO Z, et al. Application of neural network in penetration of air-breathing hypersonic missile[J]. Air & Space Defense, 2018, 1(2): 14-17(in Chinese).
|
| [16] |
赵山杉, 张雯, 李晶, 等. 基于多岛遗传算法的小型有效载荷分离装置质量优化设计[J]. 导弹与航天运载技术, 2017(2): 16-19.
ZHAO S S, ZHANG W, LI J, et al. Mass optimization design of separation devices for pint-size load based on multi-island genetic algorithm[J]. Missiles and Space Vehicles, 2017(2): 16-19(in Chinese).
|
| [17] |
张鼎逆, 刘毅. 基于改进遗传算法和序列二次规划的再入轨迹优化[J]. 浙江大学学报(工学版), 2014, 48(1): 161-167.
ZHANG D N, LIU Y. Reentry trajectory optimization based on improved genetic algorithm and sequential quadratic programming[J]. Journal of Zhejiang University(Engineering Science), 2014, 48(1): 161-167(in Chinese).
|
Figures(8) / Tables(3)
Copyright © Journal of Beijing University of Aeronautics and Astronautics
Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn
Supported by:
Beijing Renhe Information Technology Co., Ltd.
DownLoad:
