PURPOSE
The ABRIS is designed to supplement other onboard navigation systems, like the PVI-800, and to accomplish aerial navigation through: route preparation and planning, map support in all the sortie phases, processing of information from the navigational sensors, output of information to interfaced systems, navigation calculations, tactical situation display, and data link of target coordinates. The ABRIS provides:
ABRIS PANEL CONTROLS
The ABRIS controls are arranged along the bottom of the control panel and the controls include:

3-1: The ABRIS panel and controls
For the brightness and cursor manipulator knobs, you can also rotate them by clicking on them and while holding the left mouse button down, moving the mouse either side to side or up and down.
DISPLAY AND INPUT OF INFORMATION IN ABRIS
Digital and graphical information is shown in different colors on the ABRIS display depending on its function:
Message type |
Color displayed in |
Warnings |
Yellow |
Cautions |
Green |
Scales |
White |
Currently measured parameters |
White |
Mode |
Green |
Activated route |
Blue |
Data input is possible in all ABRIS operating modes: The ABRIS consists of many menus and these can be navigated through by use of the cursor manipulator (right knob on control panel) or by using the '↑' and '↓' arrow FSK buttons. Rotating the cursor manipulator clockwise moves menu item selection up and rotating it counter-clockwise moves selection of menu items down. When the cursor manipulator is used to select items from a menu, it ensures a smooth transition from one item to the next with a mandatory stop on each item. When two of the function select key (FSK) buttons are set as “Up” and “Down” arrows, these can be used to select items from a menu; one press corresponds to one item step up or down.
Input of alphanumeric values is also provided via the cursor manipulator:
TURNING ABRIS ON/OFF
After AC electrical power is supplied (ground power, batteries, or generators) and the ABRIS power switch has to be set to on, the ABRIS will start to function. Using the batteries, the AC/DC converter must set to “АВТ” (Auto position). Once turned on, the ABRIS will start an automatic self-test that can take up to 120 seconds. After the self-test is complete, the self-test page will be replaced by the MENU operating mode page. At start up, the ABRIS will automatically go through an alignment process and NAV ERROR will be displayed at the top of the MENU page in yellow until alignment is complete. To shut down the ABRIS, turn off the ABRIS power switch or remove electrical power. [0 + RSHIFT]

3-2: ABRIS in self-test mode

3-3: ABRIS MENU page after self-test and alignment
DISPLAY OF INFORMATION IN ABRIS
The ABRIS display is divided into the following areas:

3-4: Main information display areas
System Bar
The system bar is used to display current time, Global Navigation Satellite System (GNSS) sensor status, and the selected ABRIS operating mode. The system bar is displayed along the top of the display regardless of the selected operating mode. The system bar consists of the three main fields.
3-5: System bar fields
For modes that have sub-modes, the current sub-mode is indicated in the top left corner of the screen under the mode field. Navigation and GNSS messages that can be displayed in the system bar field are listed in the table below:
Message |
Meaning |
3D |
3D navigation supplied by onboard sensor |
EXCL 3D |
3D navigation with one satellite in constellation turned off manually |
PDOP 3D |
Position precision dilution |
HDOP 3D |
Bad geometric factor |
RAIM 3D |
Loss of data integrity provided to the GNSS receiver |
2D |
ABRIS is only providing 2D navigation |
ADSB 3D |
3D navigation based on data transponder |
ADSB |
Transponder mode: 2D or unknown. |
DR |
Calculations of aircraft motion parameters in case of the GNSS failure, using the last received data on the ground speed and actual track angle. This mode is used for one minute after the GNSS failure, whereupon the NAV ERROR message is displayed |
NAV ERROR |
Impossible to determine aircraft coordinates |
THRESHOLD |
If the manually entered RAIM threshold value exceeds the value suitable for the route leg: non-precision approach (0.3 nm), approach (1 nm), otherwise - 1 nm |
6-2: Navigational sensor operating mode messages Two formats can be used in the current time field: HH:MM:SS Z HH:MM:SS L In this format, НН - for hours, ММ – for minutes, and SS – for seconds. If no time zone value is entered, Greenwich Time is defaulted to; in such a case the “Z” (Zulu time) indicator appears after the time. If a time zone value is entered, the field displays local time, and the time value is followed by an “L” indicator.