NDLI: Anti-resonance control of a free-flying automated module for transportation of highly flexible pay-loads

Content Provider	IEEE Xplore Digital Library
Author	Rutkovsky, V.Yu. Sukhanov, V.M. Glumov, V.M. Dodds, S.J.
Copyright Year	2000
Description	Author affiliation: Inst. of Control Sci., Acad. of Sci., Moscow, Russia (Rutkovsky, V.Yu.)
Abstract	The synthesis of an orientation control system for a free-flying automated space module (ASM) with relay actuators, operating in the transportation regime with a flexible payload (ASM-L) is considered. The approach is based on the modal-physical dynamics model. Analysis of the "dynamics portrait" of the ASM structure is used to determine the functional relationship between the grasping point co-ordinates and the intensity of the elastic oscillations excited by the relay control torques. This function is a multi-extreme one. The global extremum (minimum) of this function is the objective function used for the optimal choice of the load grasping point co-ordinates. This is used to form an extremum-tuning loop that automatically adjusts the grasping point co-ordinates during the transportation regime. This scheme is found to be very effective in minimising the vibration amplitudes.
Starting Page	62
Ending Page	65
File Size	423122
Page Count	4
File Format	PDF
ISBN	0780364341
DOI	10.1109/COC.2000.873511
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2000-07-05
Publisher Place	Russia
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Automatic control Transportation Relays Steady-state Limit-cycles Motion control Payloads Lagrangian functions Space vehicles Equations
Content Type	Text
Resource Type	Article

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4	Project PI / Joint PI	Principal Investigator and Joint Principal Investigators of the project	Dr. B. Sutradhar bsutra@ndl.gov.in Prof. Saswat Chakrabarti will be added soon
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