Accession Number : ADA334200
Title : Aircraft Guidance and Control System Synthesis for Approach and Landing Studies.
Descriptive Note : Final rept. 1 Aug 69-31 Dec 70,
Corporate Author : LEAR SIEGLER INC OKLAHOMA CITY OK MANAGEMENT SERVICES DIV
Personal Author(s) : Kozina, John S.
PDF Url : ADA334200
Report Date : 01 JUN 1971
Pagination or Media Count : 153
Abstract : R&D Systems were synthesized and evaluated in four T-39A aircraft. Flight control and display concepts were developed to optimize navigation and guidance requirements. Successful automatic approaches through flare and touchdown were routinely accomplished even under minimum weather conditions. Thus, the systems as synthesized provided a solution to the basic problem.
Descriptors : *FLIGHT CONTROL SYSTEMS, DISPLAY SYSTEMS, LANDING AIDS, AIRCRAFT LANDINGS, INSTRUMENT LANDINGS, JET AIRCRAFT, INSTRUMENT FLIGHT, APPROACH, TRAINING AIRCRAFT, RADAR LANDING CONTROL.
Subject Categories : Flight Control and Instrumentation
Distribution Statement : APPROVED FOR PUBLIC RELEASE