Accession Number : AD0861640
Title : JB-47E Fly-By-Wire Flight Test Program.
Descriptive Note : Rept. for 1 Aug 66-15 Aug 68 on Phase 1,
Corporate Author : HYDRAULIC RESEARCH AND MFG CO BURBANK CA
Personal Author(s) : Jenney, Gavin D.
Report Date : SEP 1969
Pagination or Media Count : 76
Abstract : The report presents a description of the research investigation on a fly-by-wire control system applied to a B-47 test aircraft. The investigation is primarily confined to the pitch axis of the test aircraft and is divided into three phases. Phase I system operation is based on using an electrical non-redundant primary flight control system with control inputs being generated by the normal control motion. Phase II system operation is based upon adding a side stick controller, pitch rate and nose acceleration feedback, and electrical roll axis control to the Phase I system. Phase III incorporates a 4 channel redundant actuator with hydraulic logic into the Phase II system. Flight test of the Phase I system was completed with over 40 flight hours, including touch and go landings being accumulated on the fly-by-wire system by four different test pilots. (Author)
Descriptors : *FLIGHT CONTROL SYSTEMS), (*JET BOMBERS, REDUNDANT COMPONENTS, ELECTRIC WIRE, PITCH(MOTION), HYDRAULIC ACTUATORS, FLIGHT TESTING, AIRCRAFT LANDINGS.
Subject Categories : Bombers
Distribution Statement : APPROVED FOR PUBLIC RELEASE