FIELD: physics, navigation.
SUBSTANCE: invention relates to instrument-making and can be used in processes for controlling raw information sensors in a gimballess inertial navigation system (GINS) in ground conditions. Error estimation and control of raw information sensors in a GINS is carried out by mounting the GINS on a platform with a base and carrying out initial alignment of the GINS, followed by conversion thereof to self-contained operating mode. In said mode, the GINS is successively turned by certain banking and pitch angles, followed by pre-start check of errors of the GINS. The apparatus for implementing the method consists of a base 1 on which a platform 2 is placed for mounting the GINS to be inspected. The base 1 is in the form of a rotating frame, the rotational axis 5 of which is perpendicular to the rotational axis 7 of the rotating platform 2. On the rotational axes 5 and 7 of the base 1 and the platform 2, there are drives for setting the banking and pitch angles of the inspected GINS.
EFFECT: increased reliability.
2 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
INTEGRATED STRAPDOWN SYSTEM OF NAVIGATION OF AVERAGE ACCURACY FOR UNMANNED AERIAL VEHICLE | 2013 |
|
RU2539140C1 |
STRAPDOWN INTEGRATED NAVIGATION SYSTEM OF AVERAGE ACCURACY FOR MOBILE ONSHORE OBJECTS | 2013 |
|
RU2539131C1 |
PLATFORMLESS INERTIAL ATTITUDE-AND-HEADING REFERENCE | 2014 |
|
RU2564379C1 |
METHOD OF DETERMINING THE ANGLES OF ORIENTATION OF AN AIRCRAFT ON VERTICAL TRAJECTORIES OF FLIGHT | 2017 |
|
RU2671291C1 |
PLATFORM-FREE INERTIAL ATTITUDE AND HEADING REFERENCE SYSTEM BASED ON SENSITIVE ELEMENTS OF MEDIUM ACCURACY | 2012 |
|
RU2487318C1 |
METHOD OF PERSONAL AUTONOMOUS NAVIGATION | 2013 |
|
RU2523753C1 |
METHOD OF DETERMINING ANGULAR POSITION OF CONTROLLED DEVICE HANGED TO AIRCRAFT CARRIER | 2014 |
|
RU2553776C1 |
ADAPTIVE ATTITUDE ANGLE CORRECTOR FOR STRAPDOWN INERTIAL NAVIGATION SYSTEM | 2020 |
|
RU2749152C1 |
CORRECTION METHOD OF STRAP-DOWN INERTIAL NAVIGATION SYSTEM | 2014 |
|
RU2564380C1 |
SMALL-SIZE PLATFORMLESS INERTIAL NAVIGATION SYSTEM OF MEDIUM ACCURACY, CORRECTED FROM SYSTEM OF AIR SIGNALS | 2012 |
|
RU2502049C1 |
Authors
Dates
2015-01-10—Published
2012-12-06—Filed