Title :
Detection of aircraft-pilot-coupling caused oscillations
Author :
Koivo, A.T. ; Repperger, D.W. ; Koivo, A.J.
Author_Institution :
Purdue Univ., West Lafayette, IN, USA
Abstract :
The closed loop system consisting of an aircraft and a pilot can exhibit oscillations along any of the basic axis. These oscillations are often referred to as the pilot-induced-oscillations (PIOs) caused by the aircraft-pilot-coupling effects. For the detection of the PIOs, we propose the use of finite-state machine model. The paper discusses the identification of this model from the measurements
Keywords :
aircraft control; closed loop systems; finite state machines; identification; man-machine systems; probability; stability; aircraft-pilot-coupling; closed loop system; finite-state machine; identification; oscillations; pilot-induced-oscillations; probability; Automata; Closed loop systems; Computer crashes; Control systems; Feedback loop; Hidden Markov models; Interconnected systems; Military aircraft; Process design; Teleoperators;
Conference_Titel :
Computational Intelligence in Robotics and Automation, 1999. CIRA '99. Proceedings. 1999 IEEE International Symposium on
Conference_Location :
Monterey, CA
Print_ISBN :
0-7803-5806-6
DOI :
10.1109/CIRA.1999.810052
