Engineering PapersSearch

NASA NTRS · 19920021448

Microgravity vibration isolation: Optimal preview and feedback control

Abstract

In order to achieve adequate low-frequency vibration isolation for certain space experiments an active control is needed, due to inherent passive-isolator limitations. Proposed here are five possible state-space models for a one-dimensional vibration isolation system with a quadratic performance index. The five models are subsets of a general set of nonhomogeneous state space equations which includes disturbance terms. An optimal control is determined, using a differential equations approach, for this class of problems. This control is expressed in terms of constant, Linear Quadratic Regulator (LQR) feedback gains and constant feedforward (preview) gains. The gains can be easily determined numerically. They result in a robust controller and offers substantial improvements over a control that uses standard LQR feedback alone.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Hampton, R. D., Knospe, C. R., Grodsinsky, C. M., Allaire, P. E., Lewis, D. W.. 1992-05-01. Microgravity vibration isolation: Optimal preview and feedback control. https://ntrs.nasa.gov/citations/19920021448

Cite the original work for its findings. Save a collection to share your selection of sources.