NASA NTRS · 19880044337
Dynamics and control of a planar truss actuator
Abstract
The concept of using an active truss actuator to control the vibration of a flexible (space) structure has been investigated. The actuator with a generic beam continuum cantilevered from it has been modeled using energy methods. A time-invariant optimal state feedback scheme was utilized for the control method. A digital simulation of the system dynamic response demonstrated the good vibration control possibilities for the (planar) truss actuator on a large flexible space structure.
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Lovejoy, V. D., Robertshaw, H. H., Patten, W. N., Horner, G. C.. 1987-01-01. Dynamics and control of a planar truss actuator. https://ntrs.nasa.gov/citations/19880044337
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