DEVELOPMENT OF ON-ORBIT PREDICTIONS FOR THE MIDDECK ACTIVE CONTROL EXPERIMENT

被引：0

作者：

HOW, JP ^{[1
]}

MILLER, DW ^{[1
]}

机构：

[1] MIT,SPACE ENGN RES CTR,CAMBRIDGE,MA 02139

来源：

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

关键词：

MODELING ERRORS; ROBUST CONTROL; FLEXIBLE SPACECRAFT;

D O I：

10.1016/0967-0661(95)00103-2

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 paper presents the modeling and control design issues associated with a change in the operating environment for the Middeck Active Control Experiment (MACE): a Shuttle program scheduled to fly on STS-67, March 1995. MACE was designed to investigate the extent to which the on-orbit behavior of flexible spacecraft can be predicted and controlled using analysis and ground testing. In this paper, a refined analytic model is used to predict the on-orbit dynamics, and several techniques for estimating the on-orbit errors are discussed. Current closed-loop results using error models based on prior ground experiments predict a 35 dB performance improvement.

引用

页码：1105 / 1111

页数：7

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