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 :
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