1) orbit correction
轨道校正
1.
To meet the requirements of the BEPCII linac upgrade, the studies on beam orbit correction are carried out.
北京正负电子对撞机升级改造工程 (BEPCII)的直线注入器 (LINAC)要求建立束流轨道的自动校正系统 ,为此对束流轨道偏离的产生原因和轨道校正的方法进行了研究 ,并采用VC+ + 语言编写了相应的校正程序 ,利用最小二乘法原理对束流轨道的校正进行了模拟计算 ,取得了较为理想的结
2.
The effects of initial beam axis deviation and machine alignment errors on normalized beam emittance growth and on beam orbit offset are systematically studied, and the orbit correction with "1-to-1" correction scheme is modeled.
提出了采用“一对一”的束流轨道校正机制 ,以有效抑制这些影响 ,确保直线注入器的束流性能 。
2) orbit distortion correction
轨道畸变校正
1.
In this paper, orbit distortion corrections of the SSRF BTS lattice are done with the response matrix and SVD algorithm based on AT (matlab) toolbox.
采用基于Matlab的AT程序,利用响应矩阵和SVD算法,对SSRF高能输运线磁铁布局方案进行了轨道畸变校正,对不同的校正子和BPM放置方案作了比较研究,并对SVD算法中截断阈值的选取对输运线束流轨道畸变校正的效果作了比较研究。
4) Closed orbit distortion correction
闭合轨道畸变校正
5) closed orbit correction
闭轨校正
1.
Especially, in the process of closed orbit correction, the electron beam equilibrium orbit is shifted to the center orbit of Hefei storage ring by monitoring the closed orbit distortion due to momentum spread.
本工作对合肥储存环四极铁磁中心进行测量和闭轨校正。
6) track revising
轨迹校正
1.
To counter accumulative error of automatic tracking process, the theory of track revising and its software implements have been presented.
本文讨论了单片机控制体天文望远镜自动跟踪天体目标控制系统的理论原理及其硬件电路的实现方法,并针对自动跟踪过程中出现的累计误差进行轨迹校正,提出了校正的理论原理及其软件实现方法。
补充资料：轨道保持(见航天器轨道控制)
轨道保持(见航天器轨道控制)
orbit keeping
guidQo baoehi轨道保持(o rbit keePing)见航天器轨道控制。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条