A Generalized Second Order Compensator Design for Vibration Control of Flexible Structures
MetadataShow full item record
In this paper, a modified positive position feedback compensator design is presented for vibration control of flexible structures. The new method provides extended capability of controlling structural natural frequencies and damping. A similar compensator design where only rate sensors are available is also discussed. Ahalytical and experimental results are presented to verify the proposed method.
The article of record as published may be found at http://dx.doi.org/10.2514/6.1994-1626
Showing items related by title, author, creator and subject.
Bang, H.; Agrawal, B.N. (1994);A new approach for spacecraft maneuver based upon constraint dynamics and tracking control laws is presented in this paper. For high precision pointing requirement on spacecraft maneuver, a desired trajectory is prescribed ...
H. Chen; Agrawal, B.N. (2002);The low-frequency flexible modes of solar arrays on spacecraft are excited by the minimum-time bang-bang control during a slew maneuver. These flexible modes limit the control bandwidth and degrade the pointing error at ...
A Software-based network infrastructure for mobile ad hoc data networking in support of small tactical units using the SINCGARS radio Brand, Steven R. (Monterey, California. Naval Postgraduate School, 2006-03);Currently, there is no infrastructure in place to provide data networking capabilities to ground-based tactical units below the battalion level. Legacy, voice-centric radios, organic to these units, possesses no inherent ...