Active vibration suppression for the mast flight system

Author

Ham, Fredric M. ; Greeley, Scott W. ; Henniges, B.L.

Author_Institution

Harris Corp., Melbourne, FL, USA

Volume

9

Issue

1

fYear

1989

Firstpage

85

Lastpage

90

Abstract

Active vibration suppression of a large flexible space structure is addressed. The system (experimental test bed), performance requirements, and system simulations and models are described. The structures is a 60-m truss beam attached to the Shuttle orbiter. A baseline control system is required to provide 5% structural damping for the first ten structural (flexible) modes of the truss beam. The control design approach used to achieve the damping is a decentralized velocity feedback type. Collocated actuator and sensor locations are given, with details of the model for the proof-mass actuating device, the linear DC motor.<>

Keywords

aerospace control; large-scale systems; vibration control; 60-m truss beam; Shuttle orbiter; aerospace control; baseline control system; decentralized velocity feedback; large flexible space structure; large scale systems; linear DC motor; mast flight system; structural damping; vibration control; Control design; Control systems; DC motors; Damping; Feedback; Government; Hydraulic actuators; Joining materials; NASA; System testing;

fLanguage

English

Journal_Title

Control Systems Magazine, IEEE

Publisher

ieee

ISSN

0272-1708

Type

jour

DOI

10.1109/37.16757

Filename

16757