Abstract:
This paper describes flight test of a research external viewing device (REVD). The REVD was designed and down as a substitute for forward vision through a wind screen, co...Show MoreMetadata
Abstract:
This paper describes flight test of a research external viewing device (REVD). The REVD was designed and down as a substitute for forward vision through a wind screen, constructed of optical lenses and mirrors, and evaluated during approaches and landings. A NASA F-104 aircraft hosted the experiment to enable 25/spl deg/ glide slope approaches. Additionally, conventional 3/spl deg/ glide slope approaches were down to evaluate the REVD for a hypothetical high-speed civil transport. The REVD was satisfactory for all approaches.<>
Published in: AIAA/IEEE Digital Avionics Systems Conference. 13th DASC
Date of Conference: 30 October 1994 - 03 November 1994
Date Added to IEEE Xplore: 06 August 2002
Print ISBN:0-7803-2425-0
