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Performance validation of the ANSER control laws for the F-18 HARVThe ANSER control laws were implemented in Ada by NASA Dryden for flight test on the High Alpha Research Vehicle (HARV). The Ada implementation was tested in the hardware-in-the-loop (HIL) simulation, and results were compared to those obtained with the NASA Langley batch Fortran implementation of the control laws which are considered the 'truth model.' This report documents the performance validation test results between these implementations. This report contains the ANSER performance validation test plan, HIL versus batch time-history comparisons, simulation scripts used to generate checkcases, and detailed analysis of discrepancies discovered during testing.
Document ID
19960000083
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Messina, Michael D. (Lockheed Engineering and Sciences Co. Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1995
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-198196-PT-2
NAS 1.26:198196-PT-2
Accession Number
96N10083
Funding Number(s)
PROJECT: RTOP 505-68-30-05
CONTRACT_GRANT: NAS1-19000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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