state transition time

基本解釋

An adaptive algorithm for state-transition matrix in precise time step integration based on the Pade function is presented in this paper.
本文提出了基於逼近理論的計(jì)算精細(xì)時(shí)程積分中的狀態(tài)轉(zhuǎn)換矩陣的算法。
The state assignment is single transition time (STT), and with this method, a relatively simple set of next state equations can be obtained.
它的狀態(tài) 分配是一次轉(zhuǎn)換的（即STT），竝能得到簡(jiǎn)單的次狀態(tài)方程組。
An optimal trajectory generation strategy based on way-points is presented to solve the fixed-time state transition for spacecraft relative motion in a circular orbit.
針對(duì)圓（近圓）軌道航天器相對(duì)運(yùn)動(dòng)的固定時(shí)間狀態(tài)轉(zhuǎn)移問(wèn)題，提出了一種基於導(dǎo)航點(diǎn)的多脈沖優(yōu)化軌跡生成策略。