Somanath, S and Pradeep, S and Barai, A (1999) Vibration confinement in a generic launch vehicle. In: Journal of Guidance, Control, and Dynamics, 22 (3). pp. 500-502.Full text not available from this repository.
A controller design for vibration control and alignment maintenance at critical location is developed in a generic launch vehicle whose equipment bay (EB) houses the main inertial platform. The controller uses active control to reduce the attitude disturbance in the attitude at the EB due to elastic deformation. The vibration energy is redistributed by the technique of vibration confinement, which enables the response at the EB to reach its steady state faster in the remaining portion of the structure. (AIAA)
|Item Type:||Journal Article|
|Additional Information:||Copyright of this article belongs to American Institute of Aeronautics and Astronautics.|
|Department/Centre:||Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)|
|Date Deposited:||03 Aug 2011 06:48|
|Last Modified:||03 Aug 2011 06:48|
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