SPACECRAFT CONTROL-SYSTEM FOR THE RELATIVITY MISSION

被引：6

作者：

DOUGHERTY, H ^{[1
]}

HEGEL, D ^{[1
]}

KIRSCHENBAUM, J ^{[1
]}

VANDENBEUKEL, J ^{[1
]}

REEVE, W ^{[1
]}

机构：

[1] STANFORD UNIV,STANFORD,CA 94305

来源：

CONTROL ENGINEERING PRACTICE | 1995年 / 3卷 / 08期

关键词：

ACTUATORS; AEROSPACE CONTROL; ATTITUDE CONTROL; CLOSED-LOOP SYSTEMS; CONTROL APPLICATIONS; CONTROL SYSTEM DESIGN; CONVENTIONAL CONTROL; SATELLITE CONTROL;

D O I：

10.1016/0967-0661(95)00105-4

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

The attitude and translation control system described in this paper provides precision pointing and drag-free control to accomplish a scientific mission. The unique proportional helium thruster, which uses helium boiloff from the payload, controls thrust using pressure feedback to meet the high-accuracy requirements for force knowledge. The attitude control law torque commands are combined with the translation control law force commands through a distribution matrix to determine individual thruster commands. The Global Positioning System (GPS) is used to determine position and velocity.

引用

页码：1119 / 1123

页数：5