Integrated Satellite Navigation Equipment CN-3307

Integrated Satellite Navigation Equipment CN-3307

SNS СN-3307 user equipment is intended for interoper­ability with avionics of Su and MiG aircrafts in standalone and automatic modes.

SNS СN-3307 user equipment provides:

-   standalone desired track flight execution and ap­proach;

-   control from standard aircraft panel or from its own control unit;

-   input and storage of navigation database (WPTs, routes);

-   online storage of the current parameters;

-   input of altitude and speed parameters;

-   input of flight direction parameters;

-   output of navigation data to standard indicating de­vices;

-   output of monitoring signals to ACS (Automatic Con­trol System);

-   output of digital information on standard interfaces ARINC 429 and RS 232;

-   output of information for navigation bombing execu­tion.

SPECIFICATION

Precision of definition:
-   coordinates:
-   altitude:
-   current time:
-   ground speed vector:

UTC time mark:

track angle:


20 m;
30 m;
1 mksec;
0,2 m/sec;

100 nsec;

0,5°

* said data are provided at accelerations from –10g tо +10g, flight speed up to 3600 km/h and altitude up to 30 000 m

Supply voltage:

Power consumption:

Total weight of a complete set:

Reception and issue of information:

27 V

30 W

10,5 kg

via digital and analog interfaces of Su and MiG aircrafts.