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Conversion from Engineering Units to Telemetry Counts on Dryden Flight SimulatorsDryden real-time flight simulators encompass the simulation of pulse code modulation (PCM) telemetry signals. This paper presents a new method whereby the calibration polynomial (from first to sixth order), representing the conversion from counts to engineering units (EU), is numerically inverted in real time. The result is less than one-count error for valid EU inputs. The Newton-Raphson method is used to numerically invert the polynomial. A reverse linear interpolation between the EU limits is used to obtain an initial value for the desired telemetry count. The method presented here is not new. What is new is how classical numerical techniques are optimized to take advantage of modem computer power to perform the desired calculations in real time. This technique makes the method simple to understand and implement. There are no interpolation tables to store in memory as in traditional methods. The NASA F-15 simulation converts and transmits over 1000 parameters at 80 times/sec. This paper presents algorithm development, FORTRAN code, and performance results.
Document ID
19990004344
Acquisition Source
Armstrong Flight Research Center
Document Type
Reprint (Version printed in journal)
Authors
Fantini, Jay A.
(Woodside Summit Group, Inc. Mountain View, CA United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1998
Subject Category
Computer Programming And Software
Report/Patent Number
NASA/CR-1998-206563
NAS 1.26:206563
H-2272
Report Number: NASA/CR-1998-206563
Report Number: NAS 1.26:206563
Report Number: H-2272
Meeting Information
Meeting: International Telemetry Conference
Location: San Diego, CA
Country: United States
Start Date: October 26, 1998
End Date: October 28, 1998
Funding Number(s)
PROJECT: RTOP 314-02-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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