A simulator investigation of rolling requirements for landing approach

dc.contributor.author	A. G. Barnes	en_US
dc.date.accessioned	2014-10-21T15:50:04Z
dc.date.available	2014-10-21T15:50:04Z
dc.date.issued	1967	en_US
dc.identifier.other	ARC/R&M-3605	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/2873
dc.description.abstract	Summary. This Report describes a fixed-base simulator investigation of the rolling requirements for two types of aircraft on the landing approach. A small trainer/strike aircraft, and a large transport aircraft are simulated, and pilot opinion is obtained for differing values of damping in roll, and the maximum rolling acceleration for full aileron. The results are compared both with existing handling criteria, and also with known aircraft.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	A simulator investigation of rolling requirements for landing approach	en_US