Current research on advanced cockpit display systems
R. L. Winglade
Abstract
Open-access reader
R. L. Winglade
Abstract
Open-access reader
Current cockpit-display philosophy i s discussed i n terms of t h e p i l o t ' s informational requirements.P i l o t s ' scan p a t t e r n s obtained through t h e use of an eye-position camera and a ground-based simulator a r e depicted f o r a conventional display system and f o r two advanced concepts.Preliminary r e s u l t s of some f l i g h t -t e s t and ground-simulation evaluations of advanced concepts, such a s t o t a l l y i n t e g r a t e d displays and i n d i r e c t p i l o t viewing systems, are discussed.I N 2 O D U C T I O N With t h e increased performance of f l i g h t vehicles, a d d i t i o n a l and more exacting c o n t r o l requirements are being placed on t h e p i l o t , including an increasing demand f o r all-weather operation.increased workload, e f f e c t i v e u t i l i z a t i o n of t h e p i l o t can be achieved only through e f f e c t i v e design of the pilot-vehicle i n t e r f a c e , t h e d i s p l a y s .These d i s p l a y s must provide t h e proper information i n t h e proper form.The information required can 3e divided i n t o two categories, depending upon t h e u t i l i z a t i o n .a s s e s s t h e v e h i c l e ' s s i t u a t i o n with respect t o e i t h e r a desired end point o r some vehicle l i m i t --i s conventionally displayed i n t h e form of t h e q u a n t i t a t i v e values of vehicle performance and a t t i t u d e .The second category--information required by the p i l o t t o a s c e r t a i n what c o n t r o l inputs t o make--is usually i n t h e form of t h e d i r e c t i o n and magnitude of e r r o r of t h e c o n t r o l parameter from a preplamed or d e s i r e d condition.Although t h e parameters involved are generally t h e same, optimization of a display u n i t f o r e i t h e r category usually cannot.be accomplished without adversely a f f e c t i n g t h e d i s p l a y ' s czpa5ility i3 :he other category As a r e s u l t of t h i s The first category--information required by t h e p i l o t t oTraditionally, d i s p l a y s have been designed t o present t h e information required f o r t h e p i l o t i n g t a s k but not n e c e s s a r i l y i n a manner t h a t has made optimum u t i l i z a t i o n of the p i l o t ' s sensory c a p a b i l i t i e s .The recent development of a reasonably l i g h t and accurate eye-movement camera and t h e use of other instrumentation now affords a means of obt.aining quant.itativeinformation t h a t may be applied toward optimizing t h e p i l o t ' s d i s p l a y i n terms of both t h e mission and t h e p i l o t ' s workload.The camera records both t h e scene being viewed and t h e exact f i x a t i o n point of t h e eye on t h a t scene.The d a t a a r e i n t h e form of a real-time 16 mm movie of t h e display system with a superimposed white spot indicaking t h e p i l o t ' s eye *Head, Display and Guidance Section, NASA F l i g h
OpenAlex reports 2 citations for this work. Citation counts describe recorded attention and do not establish research quality.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
Current cockpit-display philosophy i s discussed i n terms of t h e p i l o t ' s informational requirements.P i l o t s ' scan p a t t e r n s obtained through t h e use of an eye-position camera and a ground-based simulator a r e depicted f o r a conventional display system and f o r two advanced concepts.Preliminary r e s u l t s of some f l i g h t -t e s t and ground-simulation evaluations of advanced concepts, such a s t o t a l l y i n t e g r a t e d displays and i n d i r e c t p i l o t viewing systems, are discussed.I N 2 O D U C T I O N With t h e increased performance of f l i g h t vehicles, a d d i t i o n a l and more exacting c o n t r o l requirements are being placed on t h e p i l o t , including an increasing demand f o r all-weather operation.increased workload, e f f e c t i v e u t i l i z a t i o n of t h e p i l o t can be achieved only through e f f e c t i v e design of the pilot-vehicle i n t e r f a c e , t h e d i s p l a y s .These d i s p l a y s must provide t h e proper information i n t h e proper form.The information required can 3e divided i n t o two categories, depending upon t h e u t i l i z a t i o n .a s s e s s t h e v e h i c l e ' s s i t u a t i o n with respect t o e i t h e r a desired end point o r some vehicle l i m i t --i s conventionally displayed i n t h e form of t h e q u a n t i t a t i v e values of vehicle performance and a t t i t u d e .The second category--information required by the p i l o t t o a s c e r t a i n what c o n t r o l inputs t o make--is usually i n t h e form of t h e d i r e c t i o n and magnitude of e r r o r of t h e c o n t r o l parameter from a preplamed or d e s i r e d condition.Although t h e parameters involved are generally t h e same, optimization of a display u n i t f o r e i t h e r category usually cannot.be accomplished without adversely a f f e c t i n g t h e d i s p l a y ' s czpa5ility i3 :he other category As a r e s u l t of t h i s The first category--information required by t h e p i l o t t oTraditionally, d i s p l a y s have been designed t o present t h e information required f o r t h e p i l o t i n g t a s k but not n e c e s s a r i l y i n a manner t h a t has made optimum u t i l i z a t i o n of the p i l o t ' s sensory c a p a b i l i t i e s .The recent development of a reasonably l i g h t and accurate eye-movement camera and t h e use of other instrumentation now affords a means of obt.aining quant.itativeinformation t h a t may be applied toward optimizing t h e p i l o t ' s d i s p l a y i n terms of both t h e mission and t h e p i l o t ' s workload.The camera records both t h e scene being viewed and t h e exact f i x a t i o n point of t h e eye on t h a t scene.The d a t a a r e i n t h e form of a real-time 16 mm movie of t h e display system with a superimposed white spot indicaking t h e p i l o t ' s eye *Head, Display and Guidance Section, NASA F l i g h
Key concepts: Cockpit, Computer science, Aeronautics, Engineering