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求解非线性代数方程组的一种建议方法
引用本文:杨超,洪冠新.求解非线性代数方程组的一种建议方法[J].飞行力学,1997,15(2):42-46.
作者姓名:杨超  洪冠新
作者单位:北京航空航天大学!北京,100083
摘    要:飞行动力学研究中常遇到的求解非线性代数方程组的问题,现提出一种求解实函数非线性代数方程组的组合迭代方法,以多步交替使用的方式将梯度下降法和拟牛顿代法结合起来,综合两者的优点,组成一种对大范围内偏离精确解的任意初值均能收敛,且有一定收敛速度的迭代法,通过算例,对三种方法进行了对比和分析,计算结果证明,该方法是优越的。

关 键 词:飞行动力学  非线性代数方程  迭代法

A Recommendable Method to Solve Nonlinear Algebraic Equations
Yang Chao, Hong Guanxin.A Recommendable Method to Solve Nonlinear Algebraic Equations[J].Flight Dynamics,1997,15(2):42-46.
Authors:Yang Chao  Hong Guanxin
Institution:Beijing University of Aeronautics and Astronautics
Abstract:The solution of nonlinear algebraic equations is usually met in the study of flight dynamics. A combinatorial iteration method to solve the nonlinear algebraic equations is put forward in this paper. The method combines the gradient method with quasi-Newton method and abstracts the advantages from the both methods, using them steps by steps alternately. The combinatorial method can be converged to any initial values that has long distance to the precise values and has proper speed for convergence.
Keywords:Flight dynamics Nonlinear algebraic equations Iteration method
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