Title :
The use of inertial measurement units as a primary sensor for a flight control system
Abstract :
The topics covered by the author are: what measurements are needed; what are the technology drivers; use of the technology drivers; comparison of technologies and technology changes.
Keywords :
aircraft control; accelerometers; flight control system; gyros; inertial measurement units; primary sensor; technology changes; technology drivers;
Conference_Titel :
Airborne Navigation Systems Workshop (Ref. No. 1998/275), IEE
DOI :
10.1049/ic:19980391
