NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
The dynamics and control of large flexible space structures, 6The controls analysis based on a truncated finite element model of the 122m. Hoop/Column Antenna System focuses on an analysis of the controllability as well as the synthesis of control laws. Graph theoretic techniques are employed to consider controllability for different combinations of number and locations of actuators. Control law synthesis is based on an application of the linear regulator theory as well as pole placement techniques. Placement of an actuator on the hoop can result in a noticeable improvement in the transient characteristics. The problem of orientation and shape control of an orbiting flexible beam, previously examined, is now extended to include the influence of solar radiation environmental forces. For extremely flexible thin structures modification of control laws may be required and techniques for accomplishing this are explained. Effects of environmental torques are also included in previously developed models of orbiting flexible thin platforms.
Document ID
19840002106
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bainum, P. M.
(Howard Univ. Washington, DC, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1983
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:174460
NASA-CR-174460
Report Number: NAS 1.26:174460
Report Number: NASA-CR-174460
Accession Number
84N10173
Funding Number(s)
PROJECT: RTOP 506-57-13-02
CONTRACT_GRANT: NSG-1414
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available