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Space Station man-machine automation trade-off analysis

Author: W F Zimmerman; J Bard; A Feinberg; Jet Propulsion Laboratory (U.S.)
Publisher: Pasadena, CA. : Jet Propulsion Laboratory, California Institute of Technology, [1985]
Series: NASA contractor report, NASA CR-17606.
Edition/Format:   Book   Microform : National government publication : Microfiche : English
Summary:
"The man machine automation tradeoff methodology presented is of four research tasks comprising the autonomous spacecraft system technology (ASST) project. ASST was established to identify and study system level design problems for autonomous spacecraft. Using the Space Station as an example spacecraft system requiring a certain level of autonomous control, a system level, man machine automation tradeoff methodology  Read more...
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Details

Material Type: Government publication, National government publication
Document Type: Book
All Authors / Contributors: W F Zimmerman; J Bard; A Feinberg; Jet Propulsion Laboratory (U.S.)
OCLC Number: 137287506
Notes: "February 15, 1985."
"JPL publication 85-13."
Reproduction Notes: Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1985. 2 microfiches + negative.
Description: 131 pages (various pagings) : illustrations.
Series Title: NASA contractor report, NASA CR-17606.
Responsibility: W.F. Zimmerman, J. Bard, A. Feinberg.

Abstract:

"The man machine automation tradeoff methodology presented is of four research tasks comprising the autonomous spacecraft system technology (ASST) project. ASST was established to identify and study system level design problems for autonomous spacecraft. Using the Space Station as an example spacecraft system requiring a certain level of autonomous control, a system level, man machine automation tradeoff methodology is presented that (1) optimizes man machine mixes for different ground and on orbit crew functions subject to cost, safety, weight, power, and reliability constraints, and (2) plots the best incorporation plan for new, emerging technologies by weighing cost, relative availability, reliability, safety, importance to out year missions, and ease of retrofit. A fairly straightforward approach is taken by the methodology to valuing human productivity, it is still sensitive to the important subtleties associated with designing a well integrated, man machine system. These subtleties include considerations such as crew preference to retain certain spacecraft control functions or valuing human integration decision capabilities over equivalent hardware software where appropriate."--NTRS abstract.

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