Abstract
This paper deals with the problem of active vibration suppression in a laboratory model of a large flexible space structure, using nonlinear control laws. Two different controllers for the truss structure are derived, one employing on-off air jet thrusters and the other employing piezoelectric active members as actuators, Experimental results obtained with the first controller are also given.
Full Text 
Sign-in/Register to access full text options
Sign-in/Register to access full text options 
Paper version not known
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a call
