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Vega ASV-1 Operating Manual

Page 13 

4.5 ASI Setup (Airspeed Setup)

 

Zero ASI Sensor:

This setup allows your instrument to measure the zero airspeed reading of the airspeed sensor and set a calibration value
internally for this. This is equivalent to some mechanical airspeed indicators that have an adjustment to set the needle to 
zero when the aircraft is not moving. You would use this function occasionally if you see an airspeed reading when the air-
craft is at rest. This may be caused by aging of the built in pressure sensor or related electronics. When this function is 
performed make sure that there is no air flow into the pitot tube as this would result in an incorrect internal calibration. As 
with any instrument, regular zeroing is suggested to achieve maximum performance.

ASI Unit:

Select if you want the ASI to be displayed in mph (statute miles per hour), km/h (kilometers per hour) or kts (nautical miles
per hour).

ASI Filter:

This function can be used to select the signal filter time constant. Selections are 

"NONE"

“FAST”

 or 

“SLOW”

. This 

selection influences the rate at which your ASI can change its reading. If you have an installation that suffers from strong 
turbulence at the pitot tube, select “slow”. If you have a very clean airflow in front of the pilot tube you can select “fast” 
which will give you a faster response to airspeed changes.

Содержание ASV-1

Страница 1: ...ic port is provided as well for use by high speed aircraft The ASV 1 can measure airspeed from 20mph to 250mph Version 1 20mph to 350mph Version 2 and 20mph to 320mph for the ASV 1HS High Speed versio...

Страница 2: ...an be in feet minute ft min or in meters second m s The ASV 1 measures airspeed from 20mph to 250mph Version 1 The ASV 1 measures airspeed from 20mph to 350mph Version 2 The ASV 1HS High Speed version...

Страница 3: ...nter Button Press the rotary control during the normal display screens to access the menu system Rotate anti clockwise for up down menu scrolling Rotate the rotary control during the normal display mo...

Страница 4: ...ressure readout Either in mB or in HG Altitude unit Airspeed value Airspeed unit VSI value Airspeed unit Airspeed tape Vs0 Min safe speed landing Vs1 Min safe speed normal Vfe Max flap speed Vno Max m...

Страница 5: ...t the altitude bug Press the F2 Down key to change the increment decrement unit to 50 or 500 Press the rotary control to exit and save The bug will be yellow when in the display screen and cyan when e...

Страница 6: ...y control to navi gate through the menu system 4 1 Exiting the menu system Press the F1 Up button to exit the menu system when the EXIT soft key is shown All changes made during navigation of the menu...

Страница 7: ...ored in the ASV 1 Flight Select whether you want the ASV 1 to automatically detect a flight or whether the pilot must press the F1 Up button to start stop a flight We recommend you select automatic fl...

Страница 8: ...display only ALT Calibrate This section allows for the calibration and fine tweaking of the altitude value Before you begin ensure that your calibrated and certified reference is set to the local pre...

Страница 9: ...be purchased from your MGL Avionics distributor to convert the RS232 output to a parallel Gillham output Prot Select the protocol of the serial RS232 output message The protocol can be selected betwee...

Страница 10: ...X Start of text 0x02 Address unsigned char 8bit 0x01 Message Type unsigned char 8bit 0x06 Length unsigned char 8bit Length of the data payload does not include the STX Address message type checksum or...

Страница 11: ...C2 C4 1000ft 0 0 0 0 0 0 0 0 1 0 900ft 0 0 0 0 0 0 0 1 1 0 700ft 0 0 0 0 0 0 1 1 0 0 400ft 0 0 0 0 0 0 1 0 1 1 200ft 0 0 0 0 0 1 1 0 0 1 800ft 0 0 0 0 1 1 0 0 0 1 2800ft 0 0 0 1 1 0 0 0 0 1 6800ft 0...

Страница 12: ...ry calm conditions Turbulence and thermal activity will make accurate calibration impossible Many areas have ideal conditions during early mornings or late afternoons Place the instrument in ft min fo...

Страница 13: ...is performed make sure that there is no air flow into the pitot tube as this would result in an incorrect internal calibration As with any instrument regular zeroing is suggested to achieve maximum pe...

Страница 14: ...Enter your minimum safe speed for landing your aircraft Vs Alarm This enables or disables Vs Alarm Vne Alarm This enables or disables the VNE alarm Cal During the factory calibration a factor has bee...

Страница 15: ...etup Miscellaneous Setup Backlight Select this menu option to adjust the backlight brightness Security Setup Select this menu option if you want to password protect the menu system Information This me...

Страница 16: ...This menu displays information about the altitude and airspeed sensors 5 Loading factory default settings Press and hold the F1 Up button and rotary control during power up to load the pre programmed...

Страница 17: ...flash CRC error will be displayed Reload the instruments firmware and load default settings If the error message still persists then it could possibly be an internal flash memory failure in which case...

Страница 18: ...t min to 10000ft min VSI units ft min or m s Airspeed sensor ADC resolution ASV 1 Version 1 12 bit ASV 1 Version 2 24 bit ASV 1HS 13 5bit Airspeed range ASV 1 Version 1 20mph to 250mph ASV 1 Version 2...

Страница 19: ...ld up of a pressure differential due to ram air or suction can lead to large errors of the indicated airspeed and alti tude Static ports are usually mounted at a strategic position on the rear side of...

Страница 20: ...on 1 Red 8 30Vdc power via power switch circuit breaker and fuse 2 Black Ground 3 White Blue Stripe RS232 Transmit data Firmware upgrading RS232 Altitude output 4 RS232 Receive data Firmware upgrading...

Страница 21: ...itude to parallel Gillham code converter The CNV ALT accepts RS232 serial data from a compatible MGL Avionics instrument and produces parallel Gillham codes in a format compatible with mode C transpon...

Страница 22: ...Vega ASV 1 Operating Manual Page 22 11 Dimensions...

Страница 23: ...relevant pilot s license This person has to make themselves familiar with the operation of this instrument and the effect of any possible failure or malfunction Under no circumstances does the manufa...

Страница 24: ...tical Speed Indicator VSI EMS 1 Engine Monitoring System FF 4 Fuel Computer INFO 1 Information Display G Force meter UTC and Local Time Slip Indicator Outside Air Temperature OAT Battery Voltage Curre...

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