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Six-DOF trajectory optimization for reusable launch vehicles via Gauss pseudospectral method 被引量:4
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作者 Zhen Wang Zhong Wu 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2016年第2期434-441,共8页
To be close to the practical flight process and increase the precision of optimal trajectory, a six-degree-offreedom(6-DOF) trajectory is optimized for the reusable launch vehicle(RLV) using the Gauss pseudospectr... To be close to the practical flight process and increase the precision of optimal trajectory, a six-degree-offreedom(6-DOF) trajectory is optimized for the reusable launch vehicle(RLV) using the Gauss pseudospectral method(GPM). Different from the traditional trajectory optimization problem which generally considers the RLV as a point mass, the coupling between translational dynamics and rotational dynamics is taken into account. An optimization problem is formulated to minimize a performance index subject to 6-DOF equations of motion, including translational and rotational dynamics. A two-step optimal strategy is then introduced to reduce the large calculations caused by multiple variables and convergence confinement in 6-DOF trajectory optimization. The simulation results demonstrate that the 6-DOF trajectory optimal strategy for RLV is feasible. 展开更多
关键词 reusable launch vehicle(RLV) trajectory optimization gauss pseudospectral method(GPM)
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PRECONDITIONED GAUSS-SEIDEL TYPE ITERATIVE METHOD FOR SOLVING LINEAR SYSTEMS 被引量:3
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作者 程光辉 黄廷祝 成孝予 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI 2006年第9期1275-1279,共5页
The preconditioned Gauss-Seidel type iterative method for solving linear systems, with the proper choice of the preconditioner, is presented. Convergence of the preconditioned method applied to Z-matrices is discussed... The preconditioned Gauss-Seidel type iterative method for solving linear systems, with the proper choice of the preconditioner, is presented. Convergence of the preconditioned method applied to Z-matrices is discussed. Also the optimal parameter is presented. Numerical results show that the proper choice of the preconditioner can lead to effective by the preconditioned Gauss-Seidel type iterative methods for solving linear systems. 展开更多
关键词 gauss-Seidel method preconditioned iterative method Z-MATRIX
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Laguerre-Gauss collocation method for initial value problems of second order ODEs 被引量:1
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作者 严建平 郭本瑜 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI 2011年第12期1541-1564,共24页
This paper proposes a new collocation method for initial value problems of second order ODEs based on the Laguerre-Gauss interpolation. It provides the global numerical solutions and possesses the spectral accuracy. N... This paper proposes a new collocation method for initial value problems of second order ODEs based on the Laguerre-Gauss interpolation. It provides the global numerical solutions and possesses the spectral accuracy. Numerical results demonstrate its high efficiency. 展开更多
关键词 Laguerre-gauss collocation method initial value problem second orderODEs
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A Chebyshev-Gauss Pseudospectral Method for Solving Optimal Control Problems 被引量:7
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作者 TANG Xiao-Jun WEI Jian-Li CHEN Kai 《自动化学报》 EI CSCD 北大核心 2015年第10期1778-1787,共10页
关键词 最优控制问题 切比雪夫 高斯点 伪谱法 拉格朗日插值 非线性规划问题 数值稳定性 求解
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Optimal control of attitude for coupled-rigid-body spacecraft via Chebyshev-Gauss pseudospectral method 被引量:3
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作者 Xinsheng GE Zhonggui YI Liqun CHEN 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI CSCD 2017年第9期1257-1272,共16页
The attitude optimal control problem (OCP) of a two-rigid-body space- craft with two rigid bodies coupled by a ball-in-socket joint is considered. Based on conservation of angular momentum of the system without the ... The attitude optimal control problem (OCP) of a two-rigid-body space- craft with two rigid bodies coupled by a ball-in-socket joint is considered. Based on conservation of angular momentum of the system without the external torque, a dynamic equation of three-dimensional attitude motion of the system is formulated. The attitude motion planning problem of the coupled-rigid-body spacecraft can be converted to a dis- crete nonlinear programming (NLP) problem using the Chebyshev-Gauss pseudospectral method (CGPM). Solutions of the NLP problem can be obtained using the sequential quadratic programming (SQP) algorithm. Since the collocation points of the CGPM are Chebyshev-Gauss (CG) points, the integration of cost function can be approximated by the Clenshaw-Curtis quadrature, and the corresponding quadrature weights can be calculated efficiently using the fast Fourier transform (FFT). To improve computational efficiency and numerical stability, the barycentric Lagrange interpolation is presented to substitute for the classic Lagrange interpolation in the approximation of state and con- trol variables. Furthermore, numerical float errors of the state differential matrix and barycentric weights can be alleviated using trigonometric identity especially when the number of CG points is large. A simple yet efficient method is used to avoid sensitivity to the initial values for the SQP algorithm using a layered optimization strategy from a feasible solution to an optimal solution. Effectiveness of the proposed algorithm is perfect for attitude motion planning of a two-rigid-body spacecraft coupled by a ball-in-socket joint through numerical simulation. 展开更多
关键词 coupled rigid body SPACECRAFT optimal control pseudospectral method(PM) Chebyshev-gauss (CG) point
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A Modified Precondition in the Gauss-Seidel Method
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作者 Alimohammad Nazari Sajjad Zia Borujeni 《Advances in Linear Algebra & Matrix Theory》 2012年第3期31-37,共7页
In recent years, a number of preconditioners have been applied to solve the linear systems with Gauss-Seidel method (see [1-7,10-12,14-16]). In this paper we use Sl instead of (S + Sm) and compare with M. Morimoto’s ... In recent years, a number of preconditioners have been applied to solve the linear systems with Gauss-Seidel method (see [1-7,10-12,14-16]). In this paper we use Sl instead of (S + Sm) and compare with M. Morimoto’s precondition [3] and H. Niki’s precondition [5] to obtain better convergence rate. A numerical example is given which shows the preference of our method. 展开更多
关键词 PRECONDITIONING gauss-SEIDEL method Regular SPLITTING Z-MATRIX NONNEGATIVE Matrix
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Greedy Randomized Gauss-Seidel Method with Oblique Direction
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作者 Weifeng Li Pingping Zhang 《Journal of Applied Mathematics and Physics》 2023年第4期1036-1048,共13页
For the linear least squares problem with coefficient matrix columns being highly correlated, we develop a greedy randomized Gauss-Seidel method with oblique direction. Then the corresponding convergence result is ded... For the linear least squares problem with coefficient matrix columns being highly correlated, we develop a greedy randomized Gauss-Seidel method with oblique direction. Then the corresponding convergence result is deduced. Numerical examples demonstrate that our proposed method is superior to the greedy randomized Gauss-Seidel method and the randomized Gauss-Seidel method with oblique direction. 展开更多
关键词 Oblique Direction Linear Least Squares Problem gauss-Seidel method
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Parameters Identification of Continuous-Time Hammerstein System with Advanced Gauss Pseudo spectral Method
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作者 何颖 戴明祥 +1 位作者 杨新民 易文俊 《Journal of Donghua University(English Edition)》 EI CAS 2016年第5期803-808,共6页
An advanced Gauss pseudospectral method(AGPM) was proposed to estimate the parameters of the continuous-time(CT)Hammerstein model.The nonlinear part of the Hammerstein system is approximated with pseudospectral approx... An advanced Gauss pseudospectral method(AGPM) was proposed to estimate the parameters of the continuous-time(CT)Hammerstein model.The nonlinear part of the Hammerstein system is approximated with pseudospectral approximation method.The linear part was written as a controllable canonical form to circumvent the high order time-derivative of the input and output(I/O) signals,which could multiply the measurement noise in the identification procession.Furthermore,an output error minimization was constructed for the CT Hammerstein model identification,which was then transcribed into a nonlinear programming(NLP) problem by AGPM.AGPM could converge to the true values of the CT Hammerstein model with few interpolated Legendre-Gauss(LG) nodes.Lastly,two illustrative examples were proposed to verify the accuracy and efficiency of the method. 展开更多
关键词 minimization Legendre controllable converge canonical verify transcribed interpolation derivative affine
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A GENERALIZED GAUSS-TYPE QUADRATURE FORMULA AND ITS APPLICATIONS TO PSEUDOSPECTRAL METHOD
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作者 王立联 郭本瑜 王中庆 《Numerical Mathematics A Journal of Chinese Universities(English Series)》 SCIE 2002年第2期179-196,共18页
A generalized Gauss-type quadrature formula is introduced, which assists in selection of collocation points in pseudospectral method for differential equations with two-point derivative boundary conditions. Some resul... A generalized Gauss-type quadrature formula is introduced, which assists in selection of collocation points in pseudospectral method for differential equations with two-point derivative boundary conditions. Some results on the related Jacobi interpolation are established. A pseudospectral scheme is proposed for the Kuramoto-Sivashisky equation. A skew symmetric decomposition is used for dealing with the nonlinear convection term. The stability and convergence of the proposed scheme are proved. The error estimates are obtained. Numerical results show the efficiency of this approach. 展开更多
关键词 GENERALIZED gauss-type QUADRATURE formula PSEUDOSPECTRAL method K-S equa-tion.
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Gauss-Legendre Iterative Methods and Their Applications on Nonlinear Systems and BVP-ODEs
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作者 Zhongli Liu Guoqing Sun 《Journal of Applied Mathematics and Physics》 2016年第11期2038-2046,共9页
In this paper, a group of Gauss-Legendre iterative methods with cubic convergence for solving nonlinear systems are proposed. We construct the iterative schemes based on Gauss-Legendre quadrature formula. The cubic co... In this paper, a group of Gauss-Legendre iterative methods with cubic convergence for solving nonlinear systems are proposed. We construct the iterative schemes based on Gauss-Legendre quadrature formula. The cubic convergence and error equation are proved theoretically, and demonstrated numerically. Several numerical examples for solving the system of nonlinear equations and boundary-value problems of nonlinear ordinary differential equations (ODEs) are provided to illustrate the efficiency and performance of the suggested iterative methods. 展开更多
关键词 Iterative method gauss-Legendre Quadrature Formula Nonlinear Systems Third-Order Convergence Nonlinear ODEs
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An Approximation Algorithm for the solution of astrophysics equations using rational scaled generalized Laguerre function collocation method based on transformed Hermite-Gauss nodes
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作者 Ali Pirkhedri Parisa Daneshjoo +3 位作者 Hamid Haj Seyyed Javadi Hamid Navidi Salem Khodamoradi Kamal Ghaderi 《International Journal of Astronomy and Astrophysics》 2011年第2期67-72,共6页
In this paper we propose a collocation method for solving Lane-Emden type equation which is nonlinear or-dinary differential equation on the semi-infinite domain. This equation is categorized as singular initial value... In this paper we propose a collocation method for solving Lane-Emden type equation which is nonlinear or-dinary differential equation on the semi-infinite domain. This equation is categorized as singular initial value problems. We solve this equation by the generalized Laguerre polynomial collocation method based on Her-mite-Gauss nodes. This method solves the problem on the semi-infinite domain without truncating it to a fi-nite domain and transforming domain of the problem to a finite domain. In addition, this method reduces so-lution of the problem to solution of a system of algebraic equations. 展开更多
关键词 Lane-Emden equation GENERALIZED Laguerre functions Collocation method Hermite-gauss NODES Nonlinear ODE SEMI-INFINITE
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A Modified Beam Propagation Method Based on the Galerkin Method with Hermite-Gauss Basis Functions
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作者 Xiao Jinbiao Liu Xu Cai Chun Fan Hehong Sun Xiaohan 《工程科学(英文版)》 2006年第4期97-101,共5页
A beam propagation method based on the Galerkin method with Hermite-Gauss basis functions for studying optical field propagation in weakly guiding dielectric structures is described. The selected basis functions natur... A beam propagation method based on the Galerkin method with Hermite-Gauss basis functions for studying optical field propagation in weakly guiding dielectric structures is described. The selected basis functions naturally satisfy the required boundary conditions at infinity so that the boundary truncation is avoided. The paraxial propagation equation is converted into a set of first-order ordinary differential equations, which are solved by means of standard numerical library routines. Besides, the calculation is efficient due to its small resulted matrix. The evolution of the injected field and its normalized power along the propagation distance in an asymmetric slab waveguide and directional coupler are presented, and the solutions are good agreement with those obtained by finite difference BPM, which tests the validity of the present approach. 展开更多
关键词 电子束传播 光子学综合电路 平面光波电路 有限元分析
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基于Gauss伪谱方法的高超声速飞行器再入轨迹快速优化 被引量:101
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作者 雍恩米 唐国金 陈磊 《宇航学报》 EI CAS CSCD 北大核心 2008年第6期1766-1772,共7页
基于一种求解最优控制问题的新方法—Gauss伪谱法(Gauss Pseudospectral Method-GPM),研究了高超声速飞行器滑翔式再入的快速轨迹优化问题。针对远程多约束条件下滑翔式再入轨迹优化问题的难点,提出了基于GPM的串行分段优化策略,包括三... 基于一种求解最优控制问题的新方法—Gauss伪谱法(Gauss Pseudospectral Method-GPM),研究了高超声速飞行器滑翔式再入的快速轨迹优化问题。针对远程多约束条件下滑翔式再入轨迹优化问题的难点,提出了基于GPM的串行分段优化策略,包括三个方面:(1)构造了设计变量初值生成器,获得近似最优解作为优化初值;(2)提出从可行解到最优解的串行优化策略;(3)引入平衡滑翔条件构造动态分段点,将再入轨迹分为初始下降段和滑翔段分别求解。以某高超声速再入飞行器为对象进行轨迹优化计算,仿真结果验证了本文的轨迹优化方法具有较高的精度和计算效率。 展开更多
关键词 轨迹优化 再入 gauss伪谱方法
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Gauss伪谱法的再入可达域计算方法 被引量:11
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作者 王涛 张洪波 +1 位作者 李永远 汤国建 《国防科技大学学报》 EI CAS CSCD 北大核心 2016年第3期75-80,共6页
为了加快优化速度和提高优化质量,提出一种基于Gauss伪谱法的再入可达域计算方法。鉴于再入时一般采用固定的攻角剖面,将攻角作为状态变量,仅对倾侧角进行单变量寻优。优化过程中,再入纵程被视为终端约束,以获取不同纵程下的最大横程,... 为了加快优化速度和提高优化质量,提出一种基于Gauss伪谱法的再入可达域计算方法。鉴于再入时一般采用固定的攻角剖面,将攻角作为状态变量,仅对倾侧角进行单变量寻优。优化过程中,再入纵程被视为终端约束,以获取不同纵程下的最大横程,将速度倾角视为过程约束,以消除弹道的跳跃现象。通过仿真,求解出了通用航空飞行器的再入可达域,结果与间接法的理论证明一致。 展开更多
关键词 再入 可达域 gauss伪谱法 攻角剖面 横程
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基于辛Gauss方法及预处理GMRES方法的暂态稳定性并行计算 被引量:3
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作者 温柏坚 胡佳怡 +2 位作者 郭文鑫 汪芳宗 李钦 《电力系统保护与控制》 EI CSCD 北大核心 2012年第22期19-24,共6页
将s级2s阶的辛Gauss方法用于电力系统暂态稳定性计算,提出了一种新的并行计算方法。该算法首先将微分—代数方程组经多级差分后转化为大规模非线性方程组,并利用牛顿法对其进行求解。在此基础上,利用矩阵分解方法将整体计算任务分解为... 将s级2s阶的辛Gauss方法用于电力系统暂态稳定性计算,提出了一种新的并行计算方法。该算法首先将微分—代数方程组经多级差分后转化为大规模非线性方程组,并利用牛顿法对其进行求解。在此基础上,利用矩阵分解方法将整体计算任务分解为两部分:一部分计算任务可按相应的级数或在不同的时间点上进行'解耦',因而具有完全的时间并行性;对剩下的一部分计算任务,采用预处理GMRES方法对其进行空间并行求解,并为此提出了一种新的预处理方法。利用三个不同规模的算例系统,对所提算法的收敛性进行了测试,并在GPU上对算法进行了实际测试。测试结果表明,该算法可以获得很高的加速比,可以用于大规模电网暂态稳定性的实时分析计算。 展开更多
关键词 暂态稳定性 gauss算法 并行计算 GMRES方法 W-变换 预处理 GPU
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基于Gauss伪谱法和直接打靶法结合的月球定点着陆轨道优化 被引量:17
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作者 彭祺擘 李海阳 +1 位作者 沈红新 唐国金 《国防科技大学学报》 EI CAS CSCD 北大核心 2012年第2期119-124,共6页
将一种求解最优控制问题的新方法—高斯伪谱法(Gauss Pseudospectral Method-GPM)和传统的直接打靶法有效结合,对月球着陆器定点软着陆轨道快速优化问题做出了研究。推导了高精度模型下着陆动力学方程。针对优化方法各自的特点和多约束... 将一种求解最优控制问题的新方法—高斯伪谱法(Gauss Pseudospectral Method-GPM)和传统的直接打靶法有效结合,对月球着陆器定点软着陆轨道快速优化问题做出了研究。推导了高精度模型下着陆动力学方程。针对优化方法各自的特点和多约束条件下最优月球软着陆轨道设计的难点,提出了问题求解的串行优化策略:将控制变量和终端时间一同作为优化变量,同时离散控制变量与状态变量,取较少的Gauss节点,利用GPM求解初值,初值的求解采用从可行解到最优解的串行优化策略;在Gauss节点上离散控制变量,利用直接打靶法求解精确最优解。仿真结果表明,本文提出的轨道优化方法具有较强的鲁棒性和快速收敛性。 展开更多
关键词 高斯伪谱法 直接打靶法 月球定点着陆 轨道优化 月球着陆器
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基于Gauss伪谱法的紧急避让汽车操纵逆动力学 被引量:12
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作者 刘英杰 赵又群 +1 位作者 许健雄 刘文婷 《机械工程学报》 EI CAS CSCD 北大核心 2012年第22期127-132,共6页
汽车高速紧急避让行驶安全性是汽车自主开发亟待解决的关键问题,也是汽车主动安全的前提和必要条件之一。提出一种汽车操纵逆动力学求解方法,该方法能够用于汽车高速紧急避让性能的客观评价。基于一种求解最优控制问题的新方法——Gaus... 汽车高速紧急避让行驶安全性是汽车自主开发亟待解决的关键问题,也是汽车主动安全的前提和必要条件之一。提出一种汽车操纵逆动力学求解方法,该方法能够用于汽车高速紧急避让性能的客观评价。基于一种求解最优控制问题的新方法——Gauss伪谱法(Gauss pseudospectral method,GPM),以驾驶员对汽车施加的转角输入和驱动力/制动力为控制变量,以最短时间完成双移线过程为控制目标,通过Gauss伪谱法将最优控制问题转化为非线性规划问题之后,运用序列二次规划方法求解。仿真结果表明,相对于间接法和传统直接法,Gauss伪谱法具有求解效率高,对初值依赖性小的优势。采用该方法解决汽车的最速操纵问题,边值约束和路径约束均得到很好的满足,可以客观评价不同汽车以最短时间完成双移线过程的操纵性能。通过实车试验,仿真值和试验值的变化趋势基本一致,从而验证了模型的正确性。 展开更多
关键词 汽车操纵逆动力学 gauss伪谱法 紧急避让 仿真 实车试验
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基于Gauss伪谱法的临近空间飞行器上升段轨迹优化 被引量:50
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作者 宗群 田栢苓 窦立谦 《宇航学报》 EI CAS CSCD 北大核心 2010年第7期1775-1781,共7页
综合考虑密度变化、声速变化、发动机推力变化及地球引力等因素对飞行轨迹的影响,研究了与实际飞行环境更加相符的临近空间飞行器燃料最优爬升轨迹。针对该问题在气动数据处理和优化求解上存在的困难,提出一种基于Gauss伪谱法(Gauss Pse... 综合考虑密度变化、声速变化、发动机推力变化及地球引力等因素对飞行轨迹的影响,研究了与实际飞行环境更加相符的临近空间飞行器燃料最优爬升轨迹。针对该问题在气动数据处理和优化求解上存在的困难,提出一种基于Gauss伪谱法(Gauss Pseudospectral Method,GPM)的求解策略。首先,依据气动数据特点,设计拟合模型对气动参数进行高精度拟合;其次,为避免间接法和传统直接法的缺点,将Gauss伪谱法和序贯二次规划(Sequential Quadratic Programming,SQP)相结合,对存在边值及加速度约束的轨迹优化问题进行求解,获得最优飞行轨迹。仿真结果表明,在更为真实的飞行环境下,利用GPM和SQP相结合的方法可在5.83s获得一条精度为10-4~10-6左右的飞行轨迹。 展开更多
关键词 临近空间飞行器 上升段轨迹优化 气动数据 gauss伪谱法 序贯二次规划
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采用Gauss伪谱法的小推力日-火Halo轨道转移优化设计 被引量:7
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作者 曹喜滨 张相宇 王峰 《宇航学报》 EI CAS CSCD 北大核心 2013年第8期1047-1054,共8页
针对日-地Halo轨道到日-火Halo轨道的小推力轨道转移问题,给出一种基于不变流形理论和Gauss伪谱法的优化设计方法。首先,在日心惯性坐标系中建立小推力轨道优化模型,并基于不变流形理论给出轨道转移中流形出口和入口的选择原则,应用该... 针对日-地Halo轨道到日-火Halo轨道的小推力轨道转移问题,给出一种基于不变流形理论和Gauss伪谱法的优化设计方法。首先,在日心惯性坐标系中建立小推力轨道优化模型,并基于不变流形理论给出轨道转移中流形出口和入口的选择原则,应用该原则在日-地系统中选择流形出口,在日-火系统中选择流形入口,并将其作为轨道转移的初末状态;然后基于Gauss伪谱法将最优控制问题离散化为非线性规划(NLP)问题,并采用基于逆多项式的形状算法给出了NLP初值的计算方法;最后对该轨道转移问题进行了数学仿真。仿真结果表明:Gauss伪谱法可有效用于小推力日-火Halo轨道转移的优化,且采用逆多项式形状算法得到的初值具有初始误差小,使得NLP收敛速度快的特点。 展开更多
关键词 gauss伪谱法 不变流形 HALO轨道 小推力
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解线性方程组的预条件Gauss-Seidel型迭代法 被引量:8
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作者 程光辉 黄廷祝 成孝予 《应用数学和力学》 CSCD 北大核心 2006年第9期1117-1121,共5页
给出了解线性方程组的预条件Gauss-Seidel型方法,提出了选取合适的预条件因子.并讨论了对Z-矩阵应用这种方法的收敛性,给出了收敛最快时的系数取值.最后给出数值例子,说明选取合适的预条件因子应用Gauss-Seidel方法求解线性方程组是有效的.
关键词 gauss-Seidel方法 预条件迭代法 Z-矩阵
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