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General
This manual describes the integrated autopilot functionality built into MGL Avionics EFIS systems.
This functionality is available in MGL Avionics Xtreme, Enigma, Odyssey, Voyager and “iEFIS”
EFIS systems.
Autopilot support for Xtreme EFIS systems is not currently available but under development.
Autopilot abilities
External autopilot systems
External autopilot systems can be controlled via NMEA interface (RS232 serial port 2) or
ARINC 429 interface (GPSS steering).
Capabilities depend on the external autopilot system.
Internal autopilot systems
The internal autopilot system can be configured as 1, 2 or 3 axis system providing bank, pitch and yaw control in any combination coupled to the EFIS internal or external navigation sources.
Autopilot functionality
The current release of the MGL Avionics integrated autopilot provides a one, two or three axis system intended to control ailerons, rudder and elevator.
Most systems would install a servo connected to ailerons and a second servo connected to elevator. A third servo connected as Yaw stabilizer can be of advantage for some aircraft. The yaw stabilizer can be engaged independent of the remainder of the autopilot system.
It is possible to use an external autopilot connected to the EFIS and use the built in yaw stabilizer at the same time.
Autopilot navigation sources
Available navigation sources are dependent on the type of EFIS and its installation.
Horizontal navigation sources
Horizontal navigation sources include the following:
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Magnetic compass (heading)
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Magnetic or true track derived from a GPS
Track to a waypoint using GPS
Track derived from route waypoints and followed by means of a GPS
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Table of contents
- 4 General
- 4 Autopilot abilities
- 4 External autopilot systems
- 4 Internal autopilot systems
- 4 Autopilot functionality
- 4 Autopilot navigation sources
- 4 Horizontal navigation sources
- 5 Vertical navigation sources
- 5 Yaw control sources
- 5 Autopilot requirements
- 6 Implementation differences between Enigma and Odyssey based systems.
- 6 Servos
- 6 PWM servo
- 7 Trio Avionics Digital servo
- 7 MGL Avionics Digital servo
- 8 Other servo systems
- 9 Engaging and disengaging the autopilot
- 9 Preflight check of the autopilot installation
- 10 Installation
- 10 Physical installation of the servos
- 11 Servo driven and undriven ranges
- 11 Post installation checks:
- 12 Pre-installation test flight
- 13 Possible issues and suggested solutions:
- 13 Ground based configuration of the autopilot system
- 14 Selecting MGL servos
- 15 Identifying a MGL servo
- 17 Configuring the roll (bank) servo
- 17 Bank servo direction
- 17 Target rate of turn
- 17 Bank servo torque
- 18 Bank servo Magnitude
- 18 Heading control:...
- 18 Bank neutral position trim
- 18 Bank left limit / Bank right limit
- 19 Recommended first settings:
- 20 Configuring the pitch servo
- 20 Pitch servo direction
- 20 Low ASI for climb (lower nose)
- 20 High ASI for descent (nose up)
- 21 Target VSI for ascent
- 21 Target VSI for descent
- 21 Pitch servo torque
- 21 Altitude control:...
- 21 Pitch angle control magnitude
- 22 Pitch change to VSI reaction
- 22 Pitch up limit / Pitch down limit
- 22 Recommended first settings
- 23 Configuring the Yaw servo
- 23 Engage mode
- 23 Yaw servo torque
- 23 Yaw servo magnitude
- 23 Yaw control
- 23 Yaw trim is:
- 24 Yaw left/right limit and servo center
- 25 First servo tests
- 25 Example: Bank servo test and checks
- 25 Ground based testing of the autopilot system
- 26 Test flight based calibration of the autopilot system
- 27 Adjusting the bank setups
- 27 Adjusting the pitch setups.
- 28 Basic roll and pitch angle control algorithm
- 30 Interpreting vertical aircraft movements under autopilot control
- 30 Once your autopilot is matched to your aircraft
- 30 Trouble shooting and known issues
- 30 Engine torque effects
- 31 PWM servos
- 31 Prerequisites
- 31 Servos
- 31 Autopilot messages
- 33 AP disengage – GPS AHRS
- 33 Electrical installation of servos (Navaid, Trio Avionics)
- 36 Electrical installation of servos (MGL Avionics)
- 38 MGL Servo LED indicator
- 39 Using the autopilot
- 39 Autopilot control on Voyager and Odyssey EFIS systems
- 40 Autopilot control on Enigma systems
- 40 The “extended keypad” menu
- 40 Disengaging the autopilot
- 41 Other forms of autopilot control
- 41 Autopilot behavior
- 41 Activating a GPS “Goto” when not pointing to the destination
- 41 Climbing and descending
- 42 Arriving at a waypoint or arriving at the last waypoint in a route
- 42 Autopilot response in turbulence
- 42 Engaging the autopilot if no navigation solution is selected
- 42 Engaging the autopilot if a navigation solution is active
- 43 Performing a “direct goto” or activating a route with the autopilot engaged
- 43 Using VOR or ILS as source for the autopilot
- 43 Vertical guidance sources
- 43 Autopilot usage requirements – safety checks and considerations