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MGL Avionics Artificial Horizons & Advanced Compasses Highly Innovative - Industry Leading Performance Inertial and Magnetic Sensor Products Both of the Singles display units fit straight into standard 2.25" and 3.5" instrument cut outs and utilise the same remote sensor modules (SP2/SP4/SP5 - described below). See the image of the 3.5" Velocity AV-2 display unit to the Left - the Infinity display has the same appearance, but, is smaller. Both Singles displays are useable configurable (menu selection) to show AH or heading or both in the one display. Their are a variety of other display options by menu selection. The manuals for the Velocity and 2.25" Infinity (AV-1) can be downloaded by clicking on the links below:
The sensor modules are also used with the complete range of MGL Avionics EFIS systems (with AH/heading capabilities (see table later in this page). These sensors are also available from a number of OEM users for use with their avionics. If you are using any of these sensors together with avionics not made by MGL Avionics, please view documentation from your avionics manufacturer regarding operating and installation details. View the documents available from this page as supplementary only. SP-2 magnetometer/electronic compass SP-4 AHRS (Attitude and Heading reference system) The SP-4 contains 3 MEMS gyros and 3 MEMS vibrating body accelerometers. Using a 16 bit data acquisition subsystem a powerful ARM7 32 bit processor is used SP-5 AHRS (Attitude and Heading reference system) The SP-5 contains 3 high grade RING gyros and 3 MEMS vibrating body accelerometers. Using a 16 bit data acquisition subsystem a powerful ARM7 32 bit processor is used to provide stabilized attitude information. Together with a SP-2 magnetometer on the same airtalk communications link the gyro heading can be automatically slaved to the magnetic heading.
Each of the sensor modules can be used as described and with the systems noted below: SP-2 magnetometer
SP-4, SP-5 AHRS
Inside the SP-2 magnetometer:
Inside the SP-4 AHRS:
Inside the SP-5 AHRS:
Downloadable manuals:
Please Note: Operation of Stratomaster Instruments is the responsibility of the pilot in command of the aircraft. The pilot in command has to make himself/herself familiar with the operation and limitations of the Stratomaster instrument(s) before commencing ground or flight operations. Under no circumstances does the manufacturer condone usage of this instrument for IFR operations. These instruments are designed for use in ultralight, microlight, experimental and homebuilt aircraft as well as any aircraft that permit use of such (non certified) instrumentation under general or special operating permits. Stratomaster Singles Instruments have Not been submitted to CAA or FAA or any of its agencies (or any regulatory authority in any other country) for any form of certification. Operation and installation of these instruments is subject to the relevant rules and regulations of your country and flight authority. If any of the above is not acceptable to the pilot in command he/she must refrain from operating the aircraft or remove any Stratomaster Instruments from the aircraft before commencing aircraft operations. . |
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to provide stabilized attitude information. Together with a SP-2 magnetometer on the same airtalk communications link the gyro heading can be automatically slaved to the magnetic heading. 
