Garmin Approach G5 - GPS-Enabled Golf Handheld, Инструкция по установке и Руководство пилота

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Garmin G5 Install Manual & Pilot's Guide 190-02072-00 Rev. E
98
Unit Installation
Installation Manual
Pilot's Guide
Appendix
Index
9)
Select the Autopilot Pitch Servo Configuration page to configure the servo
direction.
a)
With the Servo Direction set to Normal, the servo arm should move
clockwise to cause a nose down elevator movement and the servo arm
should move counterclockwise to cause a nose up elevator movement.
b)
With the Servo Direction set to Reverse, the servo arm should move
clockwise to cause a nose up elevator movement and the servo
arm should move counterclockwise to cause a nose down elevator
movement.
10) Select the Yaw Damper Configuration page to configure the servo direction.
a) With the Servo Direction set to Normal, the servo arm should move
clockwise to cause a nose left rudder movement and servo arm should
move counterclockwise to cause a nose right rudder movement.
b) With the Servo Direction set to Reverse, the servo arm should move
clockwise to cause a nose right rudder movement and the servo arm
should move counterclockwise to cause a nose left rudder movement.
11)
Set the Trim Motor Control to Disabled using the Autopilot Roll Servo,
Autopilot Pitch Servo, and Yaw Damper Configuration pages as applicable.
NOTE: Initial autopilot tuning is done with the trim control disabled to avoid the
autotrim function from interfering with the initial autopilot tuning.
a) By disabling the trim motor control, this will disable autotrim and
airspeed scheduled trim, but the pilot can still control trim in the aircraft
using the normal manual electric trim inputs. Autotrim and airspeed
scheduled trim will be setup later in the autopilot setup procedure.
12)
The proper minimum and maximum airspeed limits for the pitch servo can
be set in the Autopilot Pitch Servo Configuration page. The pitch servo
will lower or raise the nose of the aircraft to keep the aircraft within these
airspeed limits.
a) The minimum airspeed limit should be set above the stall speed of the
aircraft with some margin.
b) The maximum airspeed limit should be set below the never exceed
speed of the aircraft with some margin.