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compensateur de profondeur

elevator trim

industrie mécanique - iate.europa.eu

Le compensateur de profondeur était en position plein cabré, et le compensateur de direction était réglé à environ 1/3 à droite par rapport au neutre.

The elevator trim was set to full nose up, and the rudder trim was set to about 1/3 right of neutral.

général - CCMatrix (Wikipedia + CommonCrawl)

Nous ne disposons pas de luxe moderne de pilote automatique (ou même d’un compensateur de profondeur solide), il peut donc être fatiguant de voler après un certain temps.

We don’t have modern luxuries of autopilot (or really even a solid elevator trim) so it can be tiring to fly after a while.

général - CCMatrix (Wikipedia + CommonCrawl)

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Wind-tunnel investigation of a full-scale canard-configured general aviation airplane... Although primary emphasis of the investigation was placed on evaluating the aerodynamic performance and the stability and control characteristics of the basic configuration, tests were also conducted to study the following effects of varying the basic configuration: effect of Reynolds number; effect of canard; effect of outboard wing leading-edge droop; effect of center-of-gravity location; effect of elevator trim; effect of landing gear; effect of lateral-directional control; effect of power; effect of fixed transition; effect of water spray; effects of canard incidence, ...

général - core.ac.uk - PDF: hdl.handle.net

compensateur de profondeur

pitch trim

industrie mécanique - iate.europa.eu

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Air-breathing hypersonic vehicle guidance and control studies: an integrated trajectory/control analysis methodology, phase 2... Pitch trim calculations were dropped and an equatorial orbit was specified....

général - core.ac.uk - PDF: hdl.handle.net

Instrument scanning and controlling: using eye movement data to understand pilot behavior and strategies... Control inputs were tabulated according to throttle, wheel position, column, and pitch trim changes....

PDF: hdl.handle.net

Low-speed wind tunnel investigation of the static stability and control characteristics of an advanced turboprop configuration with the propellers placed over the tail... The primary unfavorable effect was a large pitch trim change which occurred with power, but the trim change could be minimized with a proper configuration design

PDF: hdl.handle.net

Review of research on guidance for recovery from pitch axis upsets... Many different forms of symbology have been investigated including, but not limited to, pitch scale depictions, attitude indicator icons, horizon symbology, attitude recovery arrows, and pitch trim indicators....

PDF: hdl.handle.net

Aerodynamic design methodology for blended wing body transport ... The idea is described as that cruise point, maximum lift to drag point and pitch trim point are in the same flight attitude....