DocumentCode
1041257
Title
Analytical Assessment of Performance, Handling Qualities, and Added Dynamics in Rotorcraft Flight Control
Author
Hess, Ronald A.
Author_Institution
Dept. of Mech. & Aeronaut. Eng., Univ. of California, Davis, CA
Volume
39
Issue
1
fYear
2009
Firstpage
262
Lastpage
271
Abstract
Data from a recent experimental study aimed at investigating the allowable errors in vehicle models for use in rotorcraft flight simulators are employed in the exercise of a pilot/vehicle analysis tool. It is demonstrated that a simplified multiaxis pilot model emulating pursuit tracking behavior can provide estimates of tracking performance and handling qualities. In an approximate manner, this model can accommodate the quality of visual cues. The experimental study also produced a limited but useful database for assessing current open-loop frequency-domain envelopes for maximum unnoticeable added dynamics. This database is employed to develop a closed-loop pilot/vehicle procedure for assessing maximum unnoticeable added dynamics with an ultimate goal of assessing the effects of ldquohigher orderrdquo vehicle dynamics on closed-loop pilot/vehicle control. The assessment of added dynamics is undertaken with a more detailed structural pilot model, emphasizing compensatory, as opposed to pursuit, tracking behavior.
Keywords
aerospace simulation; aircraft control; closed loop systems; frequency-domain analysis; helicopters; open loop systems; tracking; vehicle dynamics; closed-loop procedure; database; maximum unnoticeable added dynamics; multiaxis pilot model; open-loop frequency-domain envelope; pursuit tracking behavior; rotorcraft flight control; vehicle dynamics; visual cue; Aerodynamics; Aerospace control; Error correction; Humans; NASA; Open loop systems; Performance analysis; Stability; Vehicle dynamics; Visual databases; Aerospace simulation; helicopter control; human pilot modeling;
fLanguage
English
Journal_Title
Systems, Man and Cybernetics, Part A: Systems and Humans, IEEE Transactions on
Publisher
ieee
ISSN
1083-4427
Type
jour
DOI
10.1109/TSMCA.2008.2007943
Filename
4717833
Link To Document