Search NASASearch

NASA NTRS · 20020085394

Linear Parameter Varying Control for Actuator Failure

Abstract

A robust linear parameter varying (LPV) control synthesis is carried out for an HiMAT vehicle subject to loss of control effectiveness. The scheduling parameter is selected to be a function of the estimates of the control effectiveness factors. The estimates are provided on-line by a two-stage Kalman estimator. The inherent conservatism of the LPV design is reducing through the use of a scaling factor on the uncertainty block that represents the estimation errors of the effectiveness factors. Simulations of the controlled system with the on-line estimator show that a superior fault-tolerance can be achieved.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Shin, Jong-Yeob, Wu, N. Eva, Belcastro, Christine, Bushnell, Dennis M.. 2002-10-01. Linear Parameter Varying Control for Actuator Failure. https://ntrs.nasa.gov/citations/20020085394

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