Accession Number : ADA327418
Title : Development of Lateral-Directional Equivalent System Models for Selected U.S. Navy Tactical Aircraft.
Descriptive Note : Final rept. 1 Oct 81-30 Nov 82,
Corporate Author : NAVAL AIR DEVELOPMENT CENTER WARMINSTER PA AIRCRAFT AND CREW SYSTEMS TECHNOLO GY DIRECTORATE
Personal Author(s) : Bischoff, D. E. ; Palmer, R. E.
PDF Url : ADA327418
Report Date : SEP 1983
Pagination or Media Count : 100
Abstract : The high order transfer functions representing the lateral directional responses to pilot control inputs were matched with low order equivalent forms in the frequency domain for five Navy tactical aircraft: the A-6, A-7, S-3, F-14, and F-18. The candidate low order equivalent forms investigated were: (1) the complete three degree of freedom representation of roll and sideslip angle responses, and (2) the single degree of freedom roll mode and Dutch roll approximations. Acceptable models were generally obtained for both forms. Simultaneous matching of sideslip and roll angle responses and/or apriori information for the roots was required to match the full three degree of freedom forms. The equivalent system models are discussed in terms of their match statistics. The equivalent system modal parameters, when compared against the requirements of the military flying qualities specification, demonstrate Level 1 flying qualities for the conditions analyzed with the exception of roll angle time delay for the A-7 and F-18 airplanes. The A-7's lateral command augmentation structure results in Level 2-3 equivalent time delays, while the F-18's control force inputs produce Level 2 equivalent time delays.
Descriptors : *FIGHTER AIRCRAFT, *AERODYNAMIC STABILITY, *TACTICAL AIRCRAFT, FLIGHT CONTROL SYSTEMS, NAVAL AIRCRAFT, FREQUENCY RESPONSE.
Subject Categories : Aerodynamics
Attack and Fighter Aircraft
Distribution Statement : APPROVED FOR PUBLIC RELEASE