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A decision and control multi-axis pilot model based on an urgency for action conceptAn all digital multiple axis, multiple input, multiple output pilot model flies five different tasks in aircraft of different classes while encountering turbulence represented by the Dryden spectral model. Six degree of freedom linearized aircraft equations of motion are used together with a generalized stability augmentation system. The pilot model consists of two parts: (1) a decision maker, and (2) a control action implementer. This decision maker selects the critical variable and predicts the error at action implementation. The control action implementer decides the magnitude of control to be applied and applies it. This system has been successfully compared with hybrid/analog man in the loop simulations of the F-5, A-7, T-33, and 707 aircraft, thus validating the all digital simulation and the decision and control pilot model.
Document ID
19750025609
Document Type
Conference Paper
Authors
Pollard, J. J.
(Air Force Flight Dynamics Lab. Wright-Patterson AFB, OH, United States)
Hannen, R. A.
(Wright State Univ.)
Date Acquired
August 8, 2013
Publication Date
May 1, 1974
Publication Information
Publication: NASA. Ames Res. Center 11th Ann. Conf. on Manual Control
Subject Category
Man/System Technology And Life Support
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19750025602Analytic PrimaryEleventh Annual Conference on Manual Control
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