Date of Award
Doctor of Philosophy (PhD)
Department of Aeronautics and Astronautics
Donald L. Kunz, PhD
This research presents the development of an on line linear time periodic rotor vibration controller. The Cramer-Rao bound is developed for a linear time periodic system in order to identify the quality of identified system parameters, which are used in system models for controller development. The methods developed in this work allow model parameters can be verified for accuracy and likewise adjusted to improve controller accuracy.
DTIC Accession Number
Schulz, Christopher S., "Rotorcraft Smoothing Via Linear Time Periodic Methods" (2007). Theses and Dissertations. 2906.