Motion-base simulator evaluation of an aircraft using an external vision system (XVS)

Author

Kramer, L. ; Williams, S. ; Rehfeld, S. ; Harrison, S.

fYear

2012

fDate

14-18 Oct. 2012

Firstpage

1

Lastpage

34

Abstract

Presents a collection of slides covering the following topics: high speed civil transport; XVS display FOV; 3 second rule; collimation requirements; pitch attitude effects; head-up flight display concepts; peripheral cues effects; motion-cueing effects; piloting tasks; RMS path error; angle of attack; JAR AWO-202; Joint Aviation Requirement; All Weather Operations; landing performance data; touchdown performance; motion simulation testing; and flight test.

Keywords

aerospace computing; aerospace simulation; aircraft displays; aircraft landing guidance; aircraft testing; computer vision; head-up displays; image motion analysis; 3 second rule; JAR AWO-202; RMS path error; XVS display FOV; aircraft; all weather operations; angle-of-attack; collimation requirements; external vision system; flight test; head-up flight display concepts; high speed civil transport; joint aviation requirement; landing performance data; motion simulation testing; motion-base simulator evaluation; motion-cueing effects; peripheral cues effects; piloting tasks; pitch attitude effects; touchdown performance;

fLanguage

English

Publisher

ieee

Conference_Titel

Digital Avionics Systems Conference (DASC), 2012 IEEE/AIAA 31st

Conference_Location

Williamsburg, VA

ISSN

2155-7195

Print_ISBN

978-1-4673-1699-6

Type

conf

DOI

10.1109/DASC.2012.6382966

Filename

6382966