This paper describes the design and application of an airborne analog computer and display generator. The system was developed as an aid to investigate the interaction of display system complexity and control system complexity on pilot rating and performance for VTOL aircraft instrument landings.
In-flight research applications of an analog computer and symbol generator to determine display and control requirements for VTOL instrument landings
Advances in test measurement. ; 1975 ; Philadelphia, PA
1975-01-01
Miscellaneous
No indication
English