Model Reduction and Control of ASTREX Using Stable Fractions

Authors

Ashok Iyer, University of Nevada, Las Vegas

Document Type

Article

Publication Date

10-1996

Publication Title

IEEE Transactions on Aerospace and Electronic Systems

Volume

32

Issue

4

First page number:

1268

Last page number:

1276

Abstract

The Advanced Space Structures Technology Research Experiments (ASTREX) is a precision structure situated at the Phillips Laboratory, Edwards Air Force Base, CA. The structure is a test bed to develop, test and validate control strategies for large-angle, three axis slewing maneuversm and vibration suppression [3,4]. The facility is funded by Air Force and is supported by on-site staff. Number of investigators from universities and industries have been involved in the research pertaining to the control-structure interaction.

Keywords

Control theory; Rotational motion; Vibration (Aeronautics); Vibration--Control

Disciplines

Aerospace Engineering | Controls and Control Theory | Electrical and Computer Engineering

Language

English

Permissions

Use Find in Your Library, contact the author, or interlibrary loan to garner a copy of the item. Publisher policy does not allow archiving the final published version. If a post-print (author's peer-reviewed manuscript) is allowed and available, or publisher policy changes, the item will be deposited.

Repository Citation

Iyer, A. (1996). Model Reduction and Control of ASTREX Using Stable Fractions. IEEE Transactions on Aerospace and Electronic Systems, 32(4), 1268-1276.