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Analytic evaluation of display requirements for approach to landingA pilot-vehicle-display model is used to study information and display requirements and the effects on system performance and reliability of pilot-induced randomness, wind gusts, configurational changes, etc. A brief description of a control theoretic systems model is given and its use and validity are demonstrated by applying it in a piloted approach to landing situation. The analysis procedure assumes that the vehicle dynamics are represented by linearized equations of motion.
Document ID
19730001394
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
Kleinman, D. L. (Bolt, Beranek, and Newman, Inc. Cambridge, MA, United States)
Baron, S. (Bolt, Beranek, and Newman, Inc. Cambridge, MA, United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1972
Publication Information
Publication: NASA, Washington 7th Ann. Conf. on Manual Control
Subject Category
Biotechnology
Accession Number
73N10121
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19730001377Collected WorksSeventh Annual Conference on Manual Control
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