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
178
Pilot's Guide
Installation Manual
Pilot's Guide
Appendix
Index
2.9.1.2 FLIGHT CONTROL
Pitch and roll commands are provided to the servos based on the active flight
director modes. Yaw commands are provided by the yaw servo. Servo motor control
limits the maximum servo speed and torque. This allows the servos to be overridden
in case of an emergency.
2.9.1.3 PITCH AXIS AND TRIM
The autopilot pitch axis uses pitch rate to stabilize the aircraft pitch attitude during
flight director maneuvers. Flight director pitch commands are rate and attitude-limited,
combined with pitch damper control, and sent to the pitch servo motor. The pitch servo
measures the output effort (torque) and optionally provides this signal to the pitch trim
motor. The pitch servo commands the pitch trim motor to reduce the average pitch
servo effort.
2.9.1.3.1 r
oLL
a
xiS
The autopilot roll axis uses roll rate to stabilize aircraft roll attitude during flight
director maneuvers. The flight director roll commands are rate- and attitude-limited,
combined with roll damper control, and sent to the roll servo motor.
2.9.1.3.2 y
aw
a
xiS
The yaw damper uses yaw rate and roll attitude to dampen the aircraft’s natural
Dutch roll response. It also uses lateral acceleration to coordinate turns and reduce
or eliminate the need for the pilot to use rudder pedal force to maintain coordinated
flight during climbs and descents.