南京理工大学 能源与动力工程学院, 江苏 南京 210094
*邮箱: ballistics@126.com
收稿:2022-05-19,
网络出版:2023-09-06,
纸质出版:2023-08-30
移动端阅览
李东阳, 常思江, 王中原. 弹箭角运动的非线性吸引域估计[J]. 兵工学报, 2023,44(8):2329-2341.
Dongyang LI, Sijiang CHANG, Zhongyuan WANG. Nonlinear Region of Attraction Estimation for Projectile’s Angular Motion[J]. Acta Armamentarii, 2023, 44(8): 2329-2341.
李东阳, 常思江, 王中原. 弹箭角运动的非线性吸引域估计[J]. 兵工学报, 2023,44(8):2329-2341. DOI: 10.12382/bgxb.2022.0417.
Dongyang LI, Sijiang CHANG, Zhongyuan WANG. Nonlinear Region of Attraction Estimation for Projectile’s Angular Motion[J]. Acta Armamentarii, 2023, 44(8): 2329-2341. DOI: 10.12382/bgxb.2022.0417.
为探索平方和规划方法在弹箭非线性吸引域估计中的应用
对计及高阶静力矩的无控尾翼弹平面角运动进行多项式化处理
并开展了非线性吸引域估计
通过构造李雅普诺夫函数并利用V-s迭代算法
得到了精度较高的吸引域估计;考虑法向力系数、俯仰力矩系数、赤道阻尼力矩系数以及马格努斯力矩系数的非线性
利用平方和优化得到脉冲末端修正迫弹空间角运动的非线性吸引域估计
由此获得脉冲参数(脉冲冲量和轴向作用位置)的有效组合范围
据此形成脉冲控制弹箭的参数设计方法。研究结果表明
利用平方和规划方法估计弹箭角运动的非线性吸引域
具有较高准确性
将估计结果用于弹箭参数设计是可行和有效的。
This paper explores the application of the Sum of Squares Programming (SOSP) in the nonlinear region of attraction estimation for projectiles. Considering quantic static moment
the nonlinear planar angular motion for an unguided fin-stabilized projectile is expressed in polynomials and its region of attraction is estimated using Lyapunov functions and V-s iterative algorithm
leading to an accurate estimation. Considering the nonlinear items of normal force coefficient
pitching moment coefficient
equatorial damping moment coefficient
and Magnus moment coefficient
the nonlinear region of attraction of the spacial angular motion of a terminal trajectory corrected mortar projectile with impulses is also studied. Thus
the effective combination of impulse parameters (impulse magnitude and axial acting position) is obtained and then a method for designing impulse parameters is proposed. The findings show that the estimation of the nonlinear region of attraction for projectile’s angular motion obtained by SOSP is of relatively high accuracy. It is feasible and effective to apply the estimation to projectile design.
MURPHY C H . Free flight motion of symmetric missiles:AD0442757 [R ] . Aberdeen Proving Ground, MD , US : Ballistic Research Laboratory , 1963 .
MURPHY C H . On the quasi-linear substitution method for missile motion caused by strongly nonlinear static moment: AD0410213 [R ] . Aberdeen Proving Ground, MD , US : Ballistic Research Laboratory , 1963 .
MURPHY C H , BRADLEY J W . Nonlinear limit motions of a slightly asymmetric re-entry vehicle [J ] . AIAA Journal , 1975 , 13 ( 7 ): 851 - 857 . DOI: 10.2514/3.60459 http://doi.org/10.2514/3.60459 https://arc.aiaa.org/doi/10.2514/3.60459 https://arc.aiaa.org/doi/10.2514/3.60459
LUSARDI R J , NICOLAIDES J D , INGRAM C W . Determination of nonsymmetric aerodynamics of re-entry missiles [J ] . Journal of Spacecraft and Rockets , 1975 , 12 ( 4 ): 193 - 198 . DOI: 10.2514/3.56963 http://doi.org/10.2514/3.56963 https://arc.aiaa.org/doi/10.2514/3.56963 https://arc.aiaa.org/doi/10.2514/3.56963
MURPHY C H . Some special cases of spin-yaw lock-in [J ] . Journal of Guidance, Control, and Dynamics , 1989 , 12 ( 6 ): 771 - 776 . DOI: 10.2514/3.20480 http://doi.org/10.2514/3.20480 https://arc.aiaa.org/doi/10.2514/3.20480 https://arc.aiaa.org/doi/10.2514/3.20480
NICOLAIDES J D . A review of some recent progress in understanding catastrophic yaw: AD0654035 [R ] . Aberdeen Proving Ground, MD , US : Ballistic Research Laboratory , 1966 .
MURPHY C H , MERMAGEN W H . Flight mechanics of an elastic symmetric missile [J ] . Journal of Guidance, Control, and Dynamics , 2001 , 24 ( 6 ): 1125 - 1132 . DOI: 10.2514/2.4847 http://doi.org/10.2514/2.4847 https://arc.aiaa.org/doi/10.2514/2.4847 https://arc.aiaa.org/doi/10.2514/2.4847
NICOLAIDES J D , INGRAM C W , CLARE T A . Investigation of the nonlinear flight dynamics of ordnance weapons [J ] . Journal of Spacecraft and Rockets , 1970 , 7 ( 10 ): 1241 - 1243 . DOI: 10.2514/3.30141 http://doi.org/10.2514/3.30141 https://arc.aiaa.org/doi/10.2514/3.30141 https://arc.aiaa.org/doi/10.2514/3.30141
MURPHY C H . Instability of controlled projectiles in ascending or descending flight [J ] . Journal of Guidance, Control, and Dynamics , 1981 , 4 ( 1 ): 66 - 69 .
MC COY R L . Modern exterior ballistics: the launch and flight dynamics of symmetric projectiles [M ] . Atglen, PA , US : Schiffer Publishing , 1999 .
MOROTE J . Resonant lock-in of unguided rockets having nonlinear aerodynamic properties [C ] // Proceedings of AIAA Aerospace Sciences Meeting and Exhibit . Reno, NV, US : AIAA , 2006 : 830 .
MOROTE J . Catastrophic yaw . why, what, how? [J ] . Progress in Aerospace Sciences , 2013 , 63 : 67 - 83 . DOI: 10.1016/j.paerosci.2013.06.002 http://doi.org/10.1016/j.paerosci.2013.06.002 https://linkinghub.elsevier.com/retrieve/pii/S0376042113000559 https://linkinghub.elsevier.com/retrieve/pii/S0376042113000559
MOROTE J , MOROTE P . Catastrophic yaw of triform and cruciform-tailed missiles [J ] . Journal of Spacecraft and Rockets , 2018 , 55 ( 1 ): 245 - 248 . DOI: 10.2514/1.A33868 http://doi.org/10.2514/1.A33868 <空>
MOROTE J , LIANO G , JIMENEZ J . Nonlinear rolling motion of triform finned missiles [J ] . Journal of Spacecraft and Rockets , 2017 , 54 ( 2 ): 459 - 470 . DOI: 10.2514/1.A33764 http://doi.org/10.2514/1.A33764 https://arc.aiaa.org/doi/10.2514/1.A33764 https://arc.aiaa.org/doi/10.2514/1.A33764
LIANO G , MOROTE J , CASTILLO J L , et al . Multiple roll angle fitting of static aerodynamic coefficients of cruciform missiles [C ] // Proceedings of AIAA Atmospheric Flight Mechanics Conference . Toronto, Canada : AIAA , 2010 : 8250 .
韩子鹏 , 常思江 , 史金光 . 弹箭非线性运动理论 [M ] . 北京 : 北京理工大学出版社 , 2016 .
HAN Z P , CHANG S J , SHI J G . Nonlinear motion theory of projectile and rocket [M ] . Beijing : Beijing University of Technology Press , 2016 . (in Chinese)
李臣明 , 刘怡昕 . 转速闭锁对远程弹箭的影响 [J ] . 弹道学报 , 2010 , 22 ( 1 ): 45 - 48 .
LI C M , LIU Y X . Effect of roll locking on long-range missile [J ] . Journal of Ballistics , 2010 , 22 ( 1 ): 45 - 48 . (in Chinese)
LI D Y , CHANG S J , WANG Z Y . Analytical solutions and a novel application: insights into spin-yaw lock-in [J ] . Journal of Guidance, Control, and Dynamics , 2017 , 40 ( 6 ): 1472 - 1481 . DOI: 10.2514/1.G000804 http://doi.org/10.2514/1.G000804 https://arc.aiaa.org/doi/10.2514/1.G000804 https://arc.aiaa.org/doi/10.2514/1.G000804
CHANG S J , LI D Y . Homotopy-analysis-method-based solutions of quintic nonlinear angular motion for projectiles [J ] . Journal of Spacecraft and Rockets , 2018 , 55 ( 3 ): 669 - 680 . DOI: 10.2514/1.A33864 http://doi.org/10.2514/1.A33864 https://arc.aiaa.org/doi/10.2514/1.A33864 https://arc.aiaa.org/doi/10.2514/1.A33864
李东阳 , 常思江 , 王中原 , 等 . 正规形法在弹箭非线性运动分析中的应用 [J ] . 国防科技大学学报 , 2022 , 44 ( 2 ): 44 - 54 .
LI D Y , CHANG S J , WANG Z Y , et al . Applying the method of normal forms to projectile nonlinear motion analysis [J ] . Journal of National University of Defense Technology , 2022 , 44 ( 2 ): 44 - 54 . (in Chinese)
MURPHY C H , MERMAGEN W H . Spin-yaw lock-in of a rotationally symmetric missile [J ] . Journal of Guidance, Control, and Dynamics , 2009 , 32 ( 2 ): 378 - 383 . DOI: 10.2514/1.40052 http://doi.org/10.2514/1.40052 https://arc.aiaa.org/doi/10.2514/1.40052 https://arc.aiaa.org/doi/10.2514/1.40052
GROSS M , ROGERS J , COSTELLO M . Nonlinear stability analysis methods for guided artillery projectiles [C ] // Proceedings of AIAA Atmospheric Flight Mechanics Conference . Atlanta,GA, US : AIAA , 2014 : 2541 .
钟扬威 , 王良明 , 傅健 , 等 . 弹箭非线性角运动稳定性Hopf分岔分析 [J ] . 兵工学报 , 2015 , 36 ( 7 ): 1195 - 1202 . DOI: 10.3969/j.issn.1000-1093.2015.07.007 http://doi.org/10.3969/j.issn.1000-1093.2015.07.007 为了分析弹箭的角运动稳定性,推导了弹箭的非线性角运动方程组,给出弹箭的非线性角运动Hopf分岔分析方法。以某型火箭弹高原试验为例,选取空气密度作为分岔参数,采用霍尔维茨判据判断了系统的稳定性,并确定了分岔点。由中心流形定理对系统进行降维,计算了Hopf分岔的3阶规范形,并作出了系统的分岔图,分析了分岔参数对极限环摆幅的影响。进行了仿真验证,结果表明,采用分岔分析方法能准确判断系统的稳定性及分析系统的极限环运动。
ZHONG Y W , WANG L M , FU J , et al . Hopf bifurcation analysis of nonlinear angular motion stability of projectile [J ] . Acta Armamentarii , 2015 , 36 ( 7 ): 1195 - 1202 . (in Chinese)
杨杰 , 常思江 , 魏伟 . 带扰流片旋转稳定弹动态稳定性 [J ] . 兵工学报 , 2021 , 42 ( 8 ): 1613 - 1623 . DOI: 10.3969/j.issn.1000-1093.2021.08.005 http://doi.org/10.3969/j.issn.1000-1093.2021.08.005 为发展一种新型弹道修正弹,以带扰流片旋转稳定弹为研究对象对其进行动态稳定性分析。推导带扰流片旋转稳定弹的动力学模型并简化得到其非齐次角运动方程,求得攻角在阶跃激励下的瞬态响应和稳态响应解析解。根据非线性角运动方程分析旋转弹结构参数、飞行参数和气动参数对系统分岔特性及稳定性的影响,通过数值计算分析带扰流片旋转稳定弹的修正能力。结果表明:求得的攻角解析解具有较高的精度;气动参数对动力学系统平衡点的稳定域影响较大;扰流片的控制效率很高。研究结果为带扰流片旋转稳定弹的结构参数设计提供了参考。
YANG J , CHANG S J , WEI W . Dynamic stability of spin-stabilized projectile with spoiler [J ] . Acta Armamentarii , 2021 , 42 ( 8 ): 1613 - 1623 . (in Chinese) DOI: 10.3969/j.issn.1000-1093.2021.08.005 http://doi.org/10.3969/j.issn.1000-1093.2021.08.005 The dynamic stability of spin-stabilized projectile with spoiler is analyzed to develop a new type of trajectory correction projectile. The dynamic model of the spin-stabilized projectile with spoiler is derived and simplified to obtain its non-homogeneous angular motion equation. The analytical solutions of the transient and steady-state responses of angle of attack under step excitation are obtained by using the non-homogeneous angular motion equation. The effects of structural, flight and aerodynamic parameters on the bifurcation characteristics and stability of the system are analyzed based on the nonlinear angular motion equation. The correction ability of the spin-stabilized projectile with spoiler was analyzed by numerical calculation. The results show that the analytical solution of the angle of attack has high accuracy, the aerodynamic parameters have a great influence on the stability region of the equilibrium point of the dynamic system, and the control efficiency of the spoiler is very high.
PARRILO P A . Structured semidefinite programs and semialgebraic geometry methods in robustness and optimization [D ] . Pasadena, CA, US : California Institute of Technology , 2000 .
TAN W . Nonlinear control analysis and synthesis using sum-of-squares programming [D ] . Berkeley, CA, US : University of California , 2006 .
CHAKRABORTY A , SEILER P , BALAS G J . Nonlinear region of attraction analysis for flight control verification and validation [J ] . Control Engineering Practice , 2011 , 19 ( 4 ): 335 - 345 . DOI: 10.1016/j.conengprac.2010.12.001 http://doi.org/10.1016/j.conengprac.2010.12.001 https://linkinghub.elsevier.com/retrieve/pii/S0967066110002595 https://linkinghub.elsevier.com/retrieve/pii/S0967066110002595
BOBITI R , LAZAR M . Automated-sampling-based stability verification and DOA estimation for nonlinear systems [J ] . IEEE Transactions on Automatic Control , 2018 , 63 ( 11 ): 3659 - 3674 . DOI: 10.1109/TAC.2018.2797196 http://doi.org/10.1109/TAC.2018.2797196 https://ieeexplore.ieee.org/document/8267231/ https://ieeexplore.ieee.org/document/8267231/
PARRILO P. A . Semidefinite programming relaxations for semialgebraic problems [J ] . Mathematical Programming , 2003 , 96 ( 2 ): 293 - 320 . DOI: 10.1007/s10107-003-0387-5 http://doi.org/10.1007/s10107-003-0387-5 http://link.springer.com/10.1007/s10107-003-0387-5 http://link.springer.com/10.1007/s10107-003-0387-5
LI D Y , IGNATYEV D , TSOURDOS A , et al . Region of attraction analysis for adaptive control of wing rock system [C ] // Proceedings of the 3rd IFAC Conference on Modelling, Identification and Control of Nonlinear Systems . Tokyo, Japan : International Federation of Automatic Control (IFAC) , 2021 , 54 : 518 - 523 .
曹小兵 . 脉冲末修迫弹弹道特性分析与控制方案设计 [D ] . 南京 : 南京理工大学 , 2012 .
CAO X B . Analysis of ballistic characteristics and design of control scheme for terminal trajectory correction mortar projectile equipped with lateral impulses [D ] . Nanjing : Nanjing University of Science and Technology , 2012 . (in Chinese)
TOPCU U , PACKARD A . Local stability analysis for uncertain nonlinear systems [J ] . IEEE Transactions on Automatic Control , 2009 , 54 ( 5 ): 1042 - 1047 . DOI: 10.1109/TAC.2009.2017157 http://doi.org/10.1109/TAC.2009.2017157 http://ieeexplore.ieee.org/document/4908958/ http://ieeexplore.ieee.org/document/4908958/
KHODADADI L , SAMADI B , KHALOOZADEH H . Estimation of region of attraction for polynomial nonlinear systems: a numerical method [J ] . ISA Transactions , 2014 , 53 ( 1 ): 25 - 32 . DOI: 10.1016/j.isatra.2013.08.005 http://doi.org/10.1016/j.isatra.2013.08.005 This paper introduces a numerical method to estimate the region of attraction for polynomial nonlinear systems using sum of squares programming. This method computes a local Lyapunov function and an invariant set around a locally asymptotically stable equilibrium point. The invariant set is an estimation of the region of attraction for the equilibrium point. In order to enlarge the estimation, a subset of the invariant set defined by a shape factor is enlarged by solving a sum of squares optimization problem. In this paper, a new algorithm is proposed to select the shape factor based on the linearized dynamic model of the system. The shape factor is updated in each iteration using the computed local Lyapunov function from the previous iteration. The efficiency of the proposed method is shown by a few numerical examples. Copyright © 2013 ISA. Published by Elsevier Ltd. All rights reserved.
AHMADI A A , PARRILO P A . Converse results on existence of sum of squares lyapunov functions [C ] // Proceedings of the 2011 50th IEEE Conference on Decision and Control and European Control Conference. Orlando, FL, US IEEE , 2011 : 6516 - 6521 .
0
浏览量
273
下载量
0
CNKI被引量
关联资源
相关文章
相关作者
相关机构
京公网安备11010802024360号