An adaptive control technology for flight safety in the presence of actuator anomalies and damage

[摘要] (cont.) This methodology enables the determination of ranges of uncertainty for which a prescribed set of closed-loop requirements are satisfied. This thesis studies several one-dimensional uncertainty analyzes for two flight maneuvers that focus on the longitudinal and lateral dynamics. As compared to the baseline controller, the adaptive controller enlarges the region of safe operation by a sizable margin in all but one of the cases considered.

[发布机构] Massachusetts Institute of Technology