TY - GEN
T1 - Aircraft control surface failure accommodation utilizing linear regulation and switching control
AU - Salman, Mishah Uzziel
AU - Chang, Borchin
PY - 2013
Y1 - 2013
N2 - An actuator jam failure is mitigated using a servomechanism formulation where the failed control surface is modeled as an exogenous input to the degraded plant. The approach exploits switching control, linear output regulation, H2 control theory, and an outer-loop PI control algorithm to track a desired reference input. Application is demonstrated using the nonlinear NASA AirSTAR Generic Transport Model (GTM).
AB - An actuator jam failure is mitigated using a servomechanism formulation where the failed control surface is modeled as an exogenous input to the degraded plant. The approach exploits switching control, linear output regulation, H2 control theory, and an outer-loop PI control algorithm to track a desired reference input. Application is demonstrated using the nonlinear NASA AirSTAR Generic Transport Model (GTM).
UR - http://www.scopus.com/inward/record.url?scp=84882443589&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84882443589&partnerID=8YFLogxK
U2 - 10.1109/ICCA.2013.6564984
DO - 10.1109/ICCA.2013.6564984
M3 - Conference contribution
AN - SCOPUS:84882443589
SN - 9781467347075
T3 - IEEE International Conference on Control and Automation, ICCA
SP - 1561
EP - 1566
BT - 2013 10th IEEE International Conference on Control and Automation, ICCA 2013
T2 - 2013 10th IEEE International Conference on Control and Automation, ICCA 2013
Y2 - 12 June 2013 through 14 June 2013
ER -