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The P-POD ProjectThe programmable pilot oriented display (P-POD), a multiprocessor based flight information processing and display unit, is discussed. Communication protocols between the three Z-80 processors inside P-POD are reviewed. The interface between the video processor, P2, and the main processor, P1, was tested. Hardware and software were revised. Data flow between P1 and P2 is illustrated. While running diagnostic routines to exercise the P1/P2 interface at maximum speed an intermittent failure was observed. A check of possible noise sources or race conditions in the hardware did not reveal the source of this failure. Possible software timing problems were also fully investigated. To eliminate the effects of this type of failure a performance monitor routine was used to detect these occasional failures and correct them. The data transmission cycle between P1/P2 is either allowed to continue normal operation or is re-initialized and restarted when an error is detected.
Document ID
19820018326
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Littlefield, J. A.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
August 10, 2013
Publication Date
June 1, 1982
Publication Information
Publication: NASA. Langley Research Center Joint Univ. Program for Air Transportation Res., 1981
Subject Category
Aircraft Instrumentation
Accession Number
82N26202
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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