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弹箭与制导学报 >

2024 , Vol. 44 >Issue 3: 35 - 42

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2024.03.005

一种高超声速滑翔式导弹轨迹优化方法

  • 刘仲信 ,
  • 苗昊春 ,
  • 皇甫逸伦 ,
  • 李雅君 ,
  • 高登巍 ,
  • 付博
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  • 西安现代控制技术研究所,陕西 西安 710065
付博(1988—),男,高级工程师,硕士,研究方向:飞行器总体与控制技术。

刘仲信(1997—),男,助理工程师,硕士,研究方向:导航制导与控制技术。

收稿日期: 2023-10-17

  网络出版日期: 2024-12-28

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A Trajectory Optimization Method for Hypersonic Gliding Missile

  • LIU Zhongxin ,
  • MIAO Haochun ,
  • HUANGFU Yilun ,
  • LI Yajun ,
  • GAO Dengwei ,
  • FU Bo
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  • Xi’an Modern Control Technology Research Institute,Xi’an 710065,Shaanxi,China

Received date: 2023-10-17

  Online published: 2024-12-28

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摘要

以高斯伪谱法为基础,考虑多段多复杂约束,提出了一种面向突防任务需求,通过罚函数法处理非全程飞行高度与飞行攻角约束的高超声速滑翔式导弹轨迹优化方法。通过仿真结果可以看出,初始状态约束、控制约束、过程约束与终端状态约束均得到了有效控制,且罚函数法处理突防任务段约束相较于常规分段约束法在约束量收束方面更具备优势,能够为后续设计工作保留更多的余量。此外,仿真结果还验证了该方法在不同射程、不同发射点高度和目标点高度条件下的有效覆盖能力。

关键词： 高斯伪谱法; 性能指标; 罚函数; 轨迹优化

本文引用格式

刘仲信 , 苗昊春 , 皇甫逸伦 , 李雅君 , 高登巍 , 付博 . 一种高超声速滑翔式导弹轨迹优化方法[J]. 弹箭与制导学报, 2024 , 44(3) : 35 -42 . DOI: 10.15892/j.cnki.djzdxb.2024.03.005

Abstract

In this paper, a trajectory optimization method of hypersonic glide missile is put forward by using penalty function method to hand non full course flying height and angle of attack constraints, which is based on Gauss Pseudo-spectral Method and takes into account multi phases, multi complex constraints and penetration mission-oriented requirements and so on. Its simulation results show that all constraint indexes are effectively controlled, and the penalty function method has more advantages in handling mission segmented constraints compared to conventional segmented constraint methods, which verified the effective coverage ability of the method under different ranges, launch heights and target heights.

Key words： Gauss pseudo-spectral method; performance index; penalty function; trajectory optimization

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参考文献

原文顺序 | 文献年度倒序 | 文中引用次数倒序
[1]
杨树兴. 陆军多管火箭武器的发展与思考[J]. 兵工学报, 2016, 37(7): 1299-1305.

DOI

YANG S X. Progress and key points for guidance of multi-ple launch rocket systems[J]. Acta Armamentarii, 2016, 37(7): 1299-1305.

[2]
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 Y, YANG Z H, CUI N G. Research on ballistic optimi-zation of boost gliding missile[J]. Journal of Astronautics, 2008, 29(1): 66-71.

[3]
周浩, 陈万春, 殷兴良. 高超声速飞行器多段弹道优化设计[J]. 宇航学报, 2008, 29(4): 1205-1209.

ZHOU H, CHEN W C, YIN X L. Multistage trajectory opt-imization design for hypersonic aircraft[J]. Journal of Astronautics, 2008, 29(4): 1205-1209.

[4]
梁欣欣, 王惠, 姜威. 升力式飞行器助推段多约束弹道优化设计[J]. 弹道学报, 2022, 34(1): 17-21.

DOI

LIANG X X, WANG H, JIANG W. Optimization design of trajectory in boost phase of lift vehicle with multiconstraints[J]. Journal of Ballistics, 2022, 34(1): 17-21.

[5]
黄国强, 陆宇平, 南英. 飞行器轨迹优化数值算法综述[J]. 中国科学: 技术科学, 2012, 42(9): 1016-1036.

HUANG G Q, LU Y P, NAN Y. A survey of numerical algorithms for trajectory optimization of flight vehicles[J]. Scientia Sinica Technologica, 2012, 42(9): 1016-1036.

[6]
张远龙, 谢愈. 滑翔飞行器弹道规划与制导方法综述[J]. 航空学报, 2020, 41(1): 50-62.

ZHANG Y L, XIE Y. Review of trajectory palnning and guidance methods for gilding vehicles[J]. Acta Aeronautica Sinica, 2020, 41(1): 50-62.

[7]
LEE C H, KIM T H, TAHK M J. Design of impact anglecontrol guidance laws via high performance slidingmode control[J]. Journal of Aerospace Engineering, 2013, 227(2): 235-253

[8]
李铁鹏, 王中原, 陈琦, 等. 基于高斯伪谱法的滑翔弹道优化算法研究[J]. 弹箭与制导学报, 2014, 34(2): 113-116.

LI T P, WANG Z Y, CHEN Q, et al. Study of gliding tr-ajectory optimization algorithm based on Gauss pseudospectral method[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2014, 34(2): 113-116.

[9]
沈冠军, 冯顺山, 曹红松. 基于高斯伪谱法的有控火箭弹弹道优化方法[J]. 弹箭与制导学报, 2015, 35(4): 109-112.

SHENG G J, FENG S S, CAO H S. Trajectory optimizati-on for controllable rockets based on Gauss pseudospectral method[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2015, 35(4): 109-112.

[10]
雍恩米, 唐国金, 陈磊. 基于Gauss伪谱方法的高超声速飞行器再入轨迹快速优化[J]. 宇航学报, 2008, 29(6): 1766-1772.

YONG E M, TANG G J, CHEN L. Fast optimization of hypersonic vehicle reentry trajectory based on Gauss pseudo-spectral method[J]. Journal of Astronautics, 2008, 29(6): 1766-1772.

[11]
庞威, 谢晓方, 孙涛, 等. 基于Gauss伪谱法的制导炸弹最优弹道研究[J]. 南京理工大学学报, 2017, 41(1): 12-21.

PANG W, XIE X F, SUN T, et al. Optimization of trajecto-ry of guided bombs using Gauss pseudospectral method[J]. Journal of Nanjing University of Science and Technology, 2017, 41(1): 12-21.

[12]
谢愈, 潘亮, 谷学强, 等. 高超声速飞行器多目标复杂约束滑翔弹道优化[J]. 国防科技大学学报, 2017, 39(2): 9-17.

XIE Y, PAN L, GU X Q, et al. Gliding trajectory optimiz-ation with multiple objectives and complicated constraints fo-r hypersonic vehicles[J]. Journal of National University of Defense Technology, 2017, 39(2): 9-17.

[13]
杨志红, 徐宝华, 姚德清. 基于高斯伪谱法的吸气式高超声速飞行器爬升弹道优化研究[J]. 导航定位与授时, 2018, 5(3): 35-40.

YANG Z H, XU B H, YAO D Q. Research on climbing trajectory optimization of airbreathing hypersonic vehicle based on Gauss pseudospectral method[J]. Navigation Positioning & Timing, 2018, 5(3): 35-40.

[14]
梅映雪, 冯玥, 王容顺, 等. 高超声速飞行器多约束再入轨迹快速优化[J]. 宇航学报, 2019, 40(7): 758-767.

MEI Y X, FENG Y, WANG R S, et al. Fast optimization of reentry trajectory for hypersonic vehicles with multiple Constraints[J]. Journal of Astronautics, 2019, 40(7): 758-767.

[15]
蔺君, 何英姿, 黄盘兴. 基于改进分段Gauss伪谱法的带推力高超声速飞行器再入轨迹规划[J]. 控制理论与应用, 2019, 36(10): 1662-1671.

LIN J, HE Y Z, HUANG P X. Powered hypersonic vehicle reentry trajectory optimization based on improved multipha-se Gauss spectral method[J]. Control Theory & Applications, 2019, 36(10): 1662-1671.

[16]
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.

ZHANG P J, LIU L H, WANG J H. Optimal ascent traje-ctory design for single stage to orbit space planes based on Gauss spectral method[J]. Aerospace Contral and Application, 2017, 43(2): 13-20.

[17]
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.

YANG J, MAO R, DU F H, et al. Study on system desig-n and optimization for guided rockets using Gauss pseudosp-ectral method[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2018, 38(5): 23-26.

[18]
曲文慧, 张晗祺, 吴了泥, 等. 基于分段高斯伪谱法的组合动力飞行器火箭挂飞轨迹规划[J]. 航天控制, 2021, 39(4): 28-35.

QU W H, ZHANG H Q, WU L N, et al. The trajectory design on the captive flight test of booster rocket and the combined cycled aircraft based on segmented gauss pseudos-pectral method[J]. Aerospace Control, 2021, 39(4): 28-35.

[19]
许一蒙, 霍鹏飞, 王超, 等. 基于高斯伪谱法的枪榴弹制导算法[J]. 探测与控制学报, 2023, 45(1): 91-96.

XU Y M, HUO P F, WANG C, et al. Gauss pseudospectr-al method for smart grenade guidance[J]. Journal of Detection & Control, 2023, 45(1): 91-96.

[20]
胡锟, 张亮. 罚函数凸优化迭代算法及在无人机路径规划中的应用[J]. 计算机应用研究, 2021, 38(3): 725-728.

HU K, ZHANG L. Penalty function convex optimization iterative algorithm and its application in UAV path planning[J]. Application Research of Computers, 2021, 38(3): 725-728.

[21]
HUANGFU Y L, FAN Y H, LI G F, et al. Adaptive grouping weapon-target assignment with field-of-view angle constraint[J]. IFAC-Papersonline, 2022, 55(3): 190-195.

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