NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Performance Validation of Version 152.0 ANSER Control Laws for the F-18 HARVThe Actuated Nose Strakes for Enhanced Rolling (ANSER) Control Laws were modified as a result of Phase 3 F/A-18 High Alpha Research Vehicle (HARV) flight testing. The control law modifications for the next software release were designated version 152.0. 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 for ANSER control law version 152.0.
Document ID
19960017566
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Messina, Michael D. (Lockheed Martin Engineering and Sciences Co. Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1996
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-198250
NAS 1.26:198250
Accession Number
96N23145
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.

Related Records

There are no records associated with this record.
No Preview Available