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Existence and Stability of Standing Waves for the Nonlinear Schrödinger Equation with Combined Nonlinearities and a Partial Harmonic Potential
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作者 Wei Wang 《Journal of Applied Mathematics and Physics》 2024年第5期1606-1615,共10页
In this paper, we study the existence of standing waves for the nonlinear Schrödinger equation with combined power-type nonlinearities and a partial harmonic potential. In the L<sup>2</sup>-supercriti... In this paper, we study the existence of standing waves for the nonlinear Schrödinger equation with combined power-type nonlinearities and a partial harmonic potential. In the L<sup>2</sup>-supercritical case, we obtain the existence and stability of standing waves. Our results are complements to the results of Carles and Il’yasov’s artical, where orbital stability of standing waves have been studied for the 2D Schrödinger equation with combined nonlinearities and harmonic potential. 展开更多
关键词 nonlinear Schrödinger Equation orbital Stability Standing Waves
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Stability of Standing Waves for the Nonlinear Schrödinger Equation with Mixed Power-Type and Hartree-Type Nonlinearities
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作者 Chunyang Yan 《Journal of Applied Mathematics and Physics》 2024年第10期3439-3457,共19页
This paper studies the existence of stable standing waves for the nonlinear Schrödinger equation with Hartree-type nonlinearity i∂tψ+Δψ+| ψ |pψ+(| x |−γ∗| ψ |2)ψ=0,   (t,x)∈[ 0,T )×ℝN.Where ψ=ψ(t,... This paper studies the existence of stable standing waves for the nonlinear Schrödinger equation with Hartree-type nonlinearity i∂tψ+Δψ+| ψ |pψ+(| x |−γ∗| ψ |2)ψ=0,   (t,x)∈[ 0,T )×ℝN.Where ψ=ψ(t,x)is a complex valued function of (t,x)∈ℝ+×ℝN. The parameters N≥3, 0p4Nand 0γmin{ 4,N }. By using the variational methods and concentration compactness principle, we prove the orbital stability of standing waves. 展开更多
关键词 nonlinear Schrödinger Equation Concentration Compactness Principle orbital Stability
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Nonlinear orbital uncertainty propagation with differential algebra and Gaussian mixture model 被引量:1
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作者 Zhen-Jiang Sun Ya-Zhong Luo +1 位作者 Pierluigi di Lizia Franco Bernelli Zazzera 《Science China(Physics,Mechanics & Astronomy)》 SCIE EI CAS CSCD 2019年第3期82-92,共11页
Nonlinear uncertainty propagation is of critical importance in many application fields of astrodynamics. In this article, a framework combining the differential algebra technique and the Gaussian mixture model method ... Nonlinear uncertainty propagation is of critical importance in many application fields of astrodynamics. In this article, a framework combining the differential algebra technique and the Gaussian mixture model method is presented to accurately propagate the state uncertainty of a nonlinear system. A high-order Taylor expansion of the final state with respect to the initial deviations is firstly computed with the differential algebra technique. Then the initial uncertainty is split to a Gaussian mixture model.With the high-order state transition polynomial, each Gaussian mixture element is propagated to the final time, forming the final Gaussian mixture model. Through this framework, the final Gaussian mixture model can include the effects of high-order terms during propagation and capture the non-Gaussianity of the uncertainty, which enables a precise propagation of probability density. Moreover, the manual derivation and integration of the high-order variational equations is avoided, which makes the method versatile. The method can handle both the application of nonlinear analytical maps on any domain of interest and the propagation of initial uncertainties through the numerical integration of ordinary differential equation. The performance of the resulting tool is assessed on some typical orbital dynamic models, including the analytical Keplerian motion, the numerical J_2 perturbed motion,and a nonlinear relative motion. 展开更多
关键词 nonlinear orbit uncertainty propagation differential ALGEBRA GAUSSIAN mixture model TAYLOR expansion
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The construction of homoclinic and heteroclinic orbitals in asymmetric strongly nonlinear systems based on the Pad'e approximant 被引量:1
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作者 冯晶晶 张琪昌 王炜 《Chinese Physics B》 SCIE EI CAS CSCD 2011年第9期19-29,共11页
In this paper, the extended Pade approximant is used to construct the homoclinic and the heteroclinic trajectories in nonlinear dynamical systems that are asymmetric at origin. Meanwhile, the conservative system, the ... In this paper, the extended Pade approximant is used to construct the homoclinic and the heteroclinic trajectories in nonlinear dynamical systems that are asymmetric at origin. Meanwhile, the conservative system, the autonomous system, and the nonautonomous system equations with quadratic and cubic nonlinearities are considered. The disturbance parameter ~ is not limited to being small. The ranges of the values of the linear and the nonlinear term parameters, which are variables, can be determined when the boundary values are satisfied. New conditions for the potentiality and the convergence are posed to make it possible to solve the boundary-value problems formulated for the orbitals and to evaluate the initial amplitude values. 展开更多
关键词 BIFURCATION Pade approximant strongly nonlinearity homoclinic and heteroclinic orbitals
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A generalized Padé approximation method of solving homoclinic and heteroclinic orbits of strongly nonlinear autonomous oscillators 被引量:1
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作者 李震波 唐驾时 蔡萍 《Chinese Physics B》 SCIE EI CAS CSCD 2014年第12期78-84,共7页
An intrinsic extension of Pad′e approximation method, called the generalized Pad′e approximation method, is proposed based on the classic Pad′e approximation theorem. According to the proposed method, the numerator... An intrinsic extension of Pad′e approximation method, called the generalized Pad′e approximation method, is proposed based on the classic Pad′e approximation theorem. According to the proposed method, the numerator and denominator of Pad′e approximant are extended from polynomial functions to a series composed of any kind of function, which means that the generalized Pad′e approximant is not limited to some forms, but can be constructed in different forms in solving different problems. Thus, many existing modifications of Pad′e approximation method can be considered to be the special cases of the proposed method. For solving homoclinic and heteroclinic orbits of strongly nonlinear autonomous oscillators, two novel kinds of generalized Pad′e approximants are constructed. Then, some examples are given to show the validity of the present method. To show the accuracy of the method, all solutions obtained in this paper are compared with those of the Runge–Kutta method. 展开更多
关键词 generalized Pad′e approximation method homoclinic and heteroclinic orbits strongly nonlinear oscillators
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ORBITAL INSTABILITY OF STANDING WAVES FOR THE GENERALIZED 3D NONLOCAL NONLINEAR SCHR?DINGER EQUATIONS
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作者 甘在会 郭柏灵 蒋芯 《Acta Mathematica Scientia》 SCIE CSCD 2015年第5期1163-1188,共26页
The existence and orbital instability of standing waves for the generalized three- dimensional nonlocal nonlinear SchrSdinger equations is studied. By defining some suitable functionals and a constrained variational p... The existence and orbital instability of standing waves for the generalized three- dimensional nonlocal nonlinear SchrSdinger equations is studied. By defining some suitable functionals and a constrained variational problem, we first establish the existence of standing waves, which relys on the inner structure of the equations under consideration to overcome the drawback that nonlocal terms violate the space-scale invariance. We then show the orbital instability of standing waves. The arguments depend upon the conservation laws of the mass and of the energy. 展开更多
关键词 nonlocal nonlinear SchrSdinger equations standing waves orbital instability
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红外高光谱大气探测仪(FY-3E/HIRAS-Ⅱ)在轨数据非线性校正方法
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作者 黄硕 顾明剑 +3 位作者 胡勇 杨天杭 邵春沅 张春明 《红外与毫米波学报》 SCIE EI CAS CSCD 北大核心 2024年第1期98-105,共8页
风云三号E星(FY-3E)搭载的高光谱大气探测仪(HIRAS-Ⅱ)能够实现大气的垂直探测,具有高光谱、高灵敏度、高精度的特点。仪器在轨之后由于仪器衰减和环境变化的原因产生非线性响应,影响在轨定标精度。针对非线性响应的问题,提出了一种基... 风云三号E星(FY-3E)搭载的高光谱大气探测仪(HIRAS-Ⅱ)能够实现大气的垂直探测,具有高光谱、高灵敏度、高精度的特点。仪器在轨之后由于仪器衰减和环境变化的原因产生非线性响应,影响在轨定标精度。针对非线性响应的问题,提出了一种基于带内光谱的非线性校正方法。首先基于带外低频光谱的非线性特征求解非线性校正系数,将此系数作为初值输入到辐射定标模型中,以星上测量的黑体带内光谱与理想光谱的偏差为目标函数,通过迭代优化非线性校正系数。通过辐射定标实验得出,校正后的黑体亮温偏差明显低于未校正和基于带外光谱的校正方法。将HIRAS-Ⅱ的观测数据与IASI进行交叉比对并计算平均亮温偏差和偏差绝对值,经过带内校正法非线性校正后的亮温平均偏差为-0.13 K,优于带外校正方法。 展开更多
关键词 HIRAS-Ⅱ 非线性校正 在轨定标 带内光谱
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涡旋光束的产生研究进展
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作者 梁晓峰 李航 +3 位作者 王雅兰 荣克鹏 王一鹏 贾凯 《激光杂志》 CAS 北大核心 2024年第6期1-12,共12页
涡旋光束是一种具有螺旋型相位分布的光束,在光学操控、光学传感、光通信、显微镜和量子纠缠等领域有着广泛的应用。对涡旋光束的概念和产生方法进行了介绍。重点回顾了国内外在近五年在连续涡旋光束、脉冲涡旋光束、基于非线性效应的... 涡旋光束是一种具有螺旋型相位分布的光束,在光学操控、光学传感、光通信、显微镜和量子纠缠等领域有着广泛的应用。对涡旋光束的概念和产生方法进行了介绍。重点回顾了国内外在近五年在连续涡旋光束、脉冲涡旋光束、基于非线性效应的涡旋光束和涡旋微型激光器领域的最新进展,同时对其发展趋势进行了分析和展望。 展开更多
关键词 涡旋光束 轨道角动量 激光器 非线性效应 微型激光器
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NaB_(4)O_(6)F与RbB_(4)O_(6)F的轨道跃迁分析
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作者 李慧敏 黄以能 《伊犁师范大学学报(自然科学版)》 2024年第2期43-47,共5页
文章研究了费米能级附近以及远离费米能级情况下不同原子轨道跃迁对晶体结构带隙的贡献问题.基于VASPKIT方法,对性能优异的非线性光学晶体NaB_(4)O_(6)F和RbB_(4)O_(6)F的能带结构、跃迁偶极矩以及总联合态密度进行了计算,并结合计算结... 文章研究了费米能级附近以及远离费米能级情况下不同原子轨道跃迁对晶体结构带隙的贡献问题.基于VASPKIT方法,对性能优异的非线性光学晶体NaB_(4)O_(6)F和RbB_(4)O_(6)F的能带结构、跃迁偶极矩以及总联合态密度进行了计算,并结合计算结果分析了不同能级下各原子轨道的跃迁情况,最终确定了在-10~0 eV能量范围内,O的px、py和pz轨道对NaB_(4)O_(6)F和RbB_(4)O_(6)F的带隙起主要贡献作用. 展开更多
关键词 非线性光学晶体 VASPKIT 轨道跃迁
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空间机器人在轨桁架组装操作基于自适应模糊CNF的阻抗控制
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作者 刘东博 陈力 《力学与实践》 2024年第4期711-721,共11页
空间桁架作为空间站一类重要基础设施,在空间站建设中起着不可替代的作用。考虑到组装好的空间桁架所占空间以及火箭的运载能力,一般采用将桁架部件发射入太空并在轨道完成组装。为实现空间桁架的组装、维护等太空任务,对空间机器人在... 空间桁架作为空间站一类重要基础设施,在空间站建设中起着不可替代的作用。考虑到组装好的空间桁架所占空间以及火箭的运载能力,一般采用将桁架部件发射入太空并在轨道完成组装。为实现空间桁架的组装、维护等太空任务,对空间机器人在轨插、拔孔操作的力/位姿阻抗控制进行了研究。建立了载体姿态受控形式的空间机器人系统动力学模型;通过桁架部件插头的运动学约束,建立了插头在基连坐标系下的运动学关系。基于阻抗控制原理,根据插头位姿与其输出力之间的动态关系建立了二阶线性阻抗模型,以实现在轨插、拔孔操作过程中输出力的精确控制。提出了一种自适应模糊组合非线性反馈(composite nonlinear feedback,CNF)控制策略,通过模糊控制器拟合系统不确定参数,作为CNF控制器的补偿输入,以降低不确定参数的影响,提高位姿的控制精度。通过Lyapunov原理证明了系统的稳定性;利用仿真分析,验证了控制策略的有效性。 展开更多
关键词 空间机器人 空间桁架 在轨插拔孔操作 阻抗控制 组合非线性反馈控制
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A hyperbolic Lindstedt-Poincare method for homoclinic motion of a kind of strongly nonlinear autonomous oscillators 被引量:7
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作者 Y.Y.Chen S.H.Chen K.Y.Sze 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2009年第5期721-729,共9页
A hyperbolic Lindstedt-Poincare method is presented to determine the homoclinic solutions of a kind of nonlinear oscillators, in which critical value of the homoclinic bifurcation parameter can be determined. The gene... A hyperbolic Lindstedt-Poincare method is presented to determine the homoclinic solutions of a kind of nonlinear oscillators, in which critical value of the homoclinic bifurcation parameter can be determined. The generalized Lienard oscillator is studied in detail, and the present method's predictions are compared with those of Runge-Kutta method to illustrate its accuracy. 展开更多
关键词 Lindstedt-Poincare method Hyperbolic function nonlinear autonomous oscillator - Homoclinic orbit
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An improved nonlinear control strategy for deep space formation flying spacecraft 被引量:2
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作者 Peng Li Pingyuan Cui Hutao Cui Deep Space Exploration Research Center,Harbin Institute of Technology, 150080 Harbin, China 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2009年第6期847-856,共10页
This paper aims to provide further study on the nonlinear modeling and controller design of formation flying spacecraft in deep space missions. First, in the Sun-Earth system, the nonlinear formation dynamics for the ... This paper aims to provide further study on the nonlinear modeling and controller design of formation flying spacecraft in deep space missions. First, in the Sun-Earth system, the nonlinear formation dynamics for the circular restricted three-body problem (CRTBP) and elliptic restricted three-body problem (ERTBP) are presented. Then, with the Floquet mode method, an impulsive controller is developed to keep the Chief on the desired Halo orbit. Finally, a nonlinear adaptive control scheme based on Nonzero set- point LQR and neural network is proposed to achieve high precision formation maneuver and keeping. The simulation results indicate that the proposed nonlinear control strategy is reasonable as it considers not only the orbit keeping of the Chief, but also the formation modeling inaccuracy. Moreover, the nonlinear adaptive control scheme is effective to improve the control accuracy of the formation keeping. 展开更多
关键词 Spacecraft formation flying. Libration pointHalo orbit - nonlinear control
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Controlof Orbitand Controlof Chaosina Class of Dynamic System 被引量:1
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作者 LI Gen guo (Shanghai Institute of Applied Mathematics and Mechanics, Shanghai University) ZHU Zheng you (Shanghai Institute of Applied Mathematics and Mechanics College of Sciences, Shanghai University) 《Advances in Manufacturing》 SCIE CAS 1999年第4期263-269,共7页
The problem of control of orbit for the dynamic system x ¨+x(1-x)(x-a)=0 is discussed. Any unbounded orbit of the dynamic system can be controlled to become a bounded periodic orbit by adding a periodic step ex... The problem of control of orbit for the dynamic system x ¨+x(1-x)(x-a)=0 is discussed. Any unbounded orbit of the dynamic system can be controlled to become a bounded periodic orbit by adding a periodic step excitation to the system. By using a nonlinear feedback control law presented in this paper the chaos of the dynamic system with excitation and damping is stabilized. This method is more effectual than the linear feedback control. 展开更多
关键词 dynamic system nonlinear feedback control control of orbit control of chaos
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THE BEHAVIOR OF A CLASS OF EPIDEMIOLOGICAL MODEL WITH POPULATION DYNAMICS AND NONLINEAR INFECTIOUS RATE
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作者 董梅芳 《Journal of Southeast University(English Edition)》 EI CAS 1995年第1期91-94,共4页
In this paper, the stability of a class of epidemiolosical medel withpopulation dynamics and nonlinear infectious rate is studied. Complete conclusionsare obtained and the practical explanation for the results is given.
关键词 nonlinear EQUILIBRIUM point / clused orbit asymptotieally stability
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EXISTENCE AND STABILITY OF STANDING WAVES FOR A COUPLED NONLINEAR SCHRDINGER SYSTEM 被引量:1
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作者 曾小雨 张贻民 周焕松 《Acta Mathematica Scientia》 SCIE CSCD 2015年第1期45-70,共26页
We study the existence and stability of the standing waves of two coupled SchrSdinger equations with potentials |x|bi(bi ∈ R,i = 1, 2). Under suitable conditions on the growth of the nonlinear terms, we first est... We study the existence and stability of the standing waves of two coupled SchrSdinger equations with potentials |x|bi(bi ∈ R,i = 1, 2). Under suitable conditions on the growth of the nonlinear terms, we first establish the existence of standing waves of the SchrSdinger system by solving a L2-normalized minimization problem, then prove that the set of all minimizers of this minimization problem is stable. Finally, we obtain the least energy solutions by the Nehari method and prove that the orbit sets of these least energy solutions are unstable, which generalizes the results of [11] where b1 = b2 = 2. 展开更多
关键词 nonlinear Schrodinger system constrained variational problem standing waves orbital stubility
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Detecting Unstable Periodic Orbits in Hyperchaotic Systems Using Subspace Fixed-Point Iteration
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作者 Hidetaka ITO Yusuke MOCHIDA Akira KUMAMOTO 《Journal of Measurement Science and Instrumentation》 CAS 2010年第S1期53-56,共4页
We present a numerical method for efficiently detecting unstable periodic orbits(UPO’s)embedded in chaotic attractors of high-dimensional systems.This method,which we refer to as subspace fixed-point iteration, locat... We present a numerical method for efficiently detecting unstable periodic orbits(UPO’s)embedded in chaotic attractors of high-dimensional systems.This method,which we refer to as subspace fixed-point iteration, locates fixed points of Poincare maps using a form of fixed-point iteration that splits the phase space into appropriate subspaces.In this paper,among a number of possible implementations,we primarily focus on a subspace method based on the Schmelcher-Diakonos(SD)method that selectively locates UPO’s by varying a stabilizing matrix,and present some applications of the resulting subspace SD method to hyperchaotic attractors where the UPO’s have more than one unstable direction. 展开更多
关键词 nonlinear dynamics CHAOS unstable periodic orbits numerical analysis SUBSPACES
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Kink wave determined by parabola solution of a nonlinear ordinary differential equation
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作者 李继彬 黎明 纳静 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI 2007年第7期883-892,共10页
By finding a parabola solution connecting two equilibrium points of a planar dynamical system, the existence of the kink wave solution for 6 classes of nonlinear wave equations is shown. Some exact explicit parametric... By finding a parabola solution connecting two equilibrium points of a planar dynamical system, the existence of the kink wave solution for 6 classes of nonlinear wave equations is shown. Some exact explicit parametric representations of kink wave solutions are given. Explicit parameter conditions to guarantee the existence of kink wave solutions are determined. 展开更多
关键词 kink wave solution connecting orbit parabola solution nonlinear wave equation nonlinear evolution equation
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具有高阶色散和立方-五次非线性项的薛定谔方程的孤立波的保持性
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作者 高晓涵 李威 《北京化工大学学报(自然科学版)》 CAS CSCD 北大核心 2023年第6期119-123,共5页
研究了具有高阶色散项和立方-五次非线性项的薛定谔方程(NLSE)在扰动下孤立波解的保持性。通过行波变换将NLSE转化为平面动力系统,由Melnikov方法得到混沌阈值,通过分岔图、最大Lyapunov指数和Poincaré截面图验证了该系统存在Smal... 研究了具有高阶色散项和立方-五次非线性项的薛定谔方程(NLSE)在扰动下孤立波解的保持性。通过行波变换将NLSE转化为平面动力系统,由Melnikov方法得到混沌阈值,通过分岔图、最大Lyapunov指数和Poincaré截面图验证了该系统存在Smale马蹄意义下的混沌,从而在参数选择时规避该区域来获得孤立波的保持区域。 展开更多
关键词 非线性薛定谔方程 MELNIKOV方法 同宿轨 混沌
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月面起飞快速交会远程导引制导律设计
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作者 王高阳 胡海霞 +1 位作者 解永春 刘涛 《空间控制技术与应用》 CSCD 北大核心 2023年第2期20-29,共10页
针对月面起飞后的快速交会远程导引任务,设计一种基于高斯摄动方程的双脉冲制导策略.首先推导了轨道修正的控制方程,然后结合远程导引的时间约束方程推导出了双脉冲制导的非线性方程组.为了获得速度增量最小解,设计规划变量,将非线性方... 针对月面起飞后的快速交会远程导引任务,设计一种基于高斯摄动方程的双脉冲制导策略.首先推导了轨道修正的控制方程,然后结合远程导引的时间约束方程推导出了双脉冲制导的非线性方程组.为了获得速度增量最小解,设计规划变量,将非线性方程组的求解问题转化为非线性规划问题,并通过序列二次规划算法对最优解进行求解.为了提高制导精度,采用迭代修正的方法对制导过程进行优化.最后,通过数据仿真,对基于高斯摄动方程的双脉冲制导策略的正确性进行校验,并与Lambert直接转移策略进行了比对.仿真结果表明,相比于Lambert直接转移制导策略,基于高斯摄动方程的双脉冲制导策略可以有效地完成快速交会远程导引任务,制导精度和燃料消耗得到了改善. 展开更多
关键词 月球轨道快速交会远程导引 高斯摄动方程 非线性规划 Lambert制导
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基于非线性相对运动方程的碰撞规避机动规划方法
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作者 李佩钰 杨震 罗亚中 《载人航天》 CSCD 北大核心 2023年第5期581-589,共9页
针对空间目标数量急剧增加带来的航天器碰撞风险增加问题,提出基于解析非线性相对运动方程的碰撞规避机动规划方法。首先,基于航天器控前飞行轨迹的精密星历及相对运动坐标系下的解析非线性相对运动方程,建立控后飞行轨迹的快速构建方法... 针对空间目标数量急剧增加带来的航天器碰撞风险增加问题,提出基于解析非线性相对运动方程的碰撞规避机动规划方法。首先,基于航天器控前飞行轨迹的精密星历及相对运动坐标系下的解析非线性相对运动方程,建立控后飞行轨迹的快速构建方法;其次,利用两目标接近数值分析算法,基于等效距离指标对航天器控后飞行轨迹与已编目空间目标的碰撞风险进行快速评估;最后,以变轨时刻及半长轴控制量为优化变量,以总速度增量最小为目标函数,以控后飞行轨迹的接近距离大于给定门限值为约束条件,建立碰撞规避机动优化模型。通过对实际任务背景的算例分析表明,提出方法得到的碰撞规避机动方案可有效降低碰撞风险。 展开更多
关键词 轨道控制 机动规划 碰撞规避 非线性相对运动
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