对任意高周期轨道控制方法的尝试

An Attempt of the Controlling Method of the Arbitrary HighPeriod Orbit

应用本征矩阵、本征值、本征矢方法（ＥＥＳ）把Ｏｔ．Ｇｒｅｂｏｇｉ和Ｙｏｒｋｅ（ＯＧＹ）控制理论转变成几个适用的表达式，并用它成功地控制了周期１、周期２等不稳定周期轨道．

Period 1、Period 2、and other periods are successfully controlled by using several practical expressions of eigenmatrixeigenvalueeigenvector (EES) scheme according to the controlling theory of Ott.Grebogi and Yorke (OGY).