FIELD: physics.
SUBSTANCE: integrated navigation channel based on a physical integration filter (PIF) is formed in an inertial navigation system (INS) with an additional autonomous channel. Self-integration of characteristic velocities of the autonomous and corrected INS is provided in the PIF. Errors of the INS are continuously corrected.
EFFECT: increased accuracy.
3 cl, 8 dwg, 5 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| INERTIAL SATELLITE NAVIGATION SYSTEM | 2003 |
|
RU2233431C1 |
| METHOD FOR SELF-CORRECTION OF SATELLITE NAVIGATION RECEIVERS AND DEVICE FOR ITS IMPLEMENTATION | 2022 |
|
RU2794703C1 |
| INERTIAL SATELLITE NAVIGATION SYSTEM | 1998 |
|
RU2148796C1 |
| METHOD OF INTEGRATION OF INTERNAL NAVIGATION SYSTEMS AND COMPLEX NAVIGATION SYSTEM | 1993 |
|
RU2082098C1 |
| SHIP NAVIGATION SYSTEM | 2011 |
|
RU2478187C2 |
| INERTIAL RADIO NAVIGATION SYSTEM | 2013 |
|
RU2539846C1 |
| STRAPDOWN INTEGRATED NAVIGATION SYSTEM OF AVERAGE ACCURACY FOR MOBILE ONSHORE OBJECTS | 2013 |
|
RU2539131C1 |
| METHOD TO IMPROVE ACCURACY OF PLATFORMLESS INERTIAL NAVIGATION SYSTEM | 2019 |
|
RU2725029C1 |
| INTEGRATED STRAPDOWN SYSTEM OF NAVIGATION OF AVERAGE ACCURACY FOR UNMANNED AERIAL VEHICLE | 2013 |
|
RU2539140C1 |
| SMALL-SIZE PLATFORMLESS INERTIAL NAVIGATION SYSTEM OF MEDIUM ACCURACY, CORRECTED FROM SYSTEM OF AIR SIGNALS | 2012 |
|
RU2502049C1 |
Authors
Dates
2010-04-10—Published
2009-02-06—Filed