FIELD: navigation.
SUBSTANCE: system comprises three accelerometers, two pickups of angular velocity connected with the computing unit, and two imitators connected to the external correcting device and external free gyroscope.
EFFECT: simplified design.
3 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF DETERMINING ANGULAR POSITION OF CONTROLLED DEVICE HANGED TO AIRCRAFT CARRIER | 2014 |
|
RU2553776C1 |
METHOD OF EVALUATION OF NAVIGATION PARAMETERS OF OPERATED MOBILE OBJECTS AND RELATED DEVICE FOR IMPLEMENTATION THEREOF | 2007 |
|
RU2339002C1 |
METHOD TO CALIBRATE SENSITIVE ELEMENTS OF PLATFORM-FREE INERTIAL NAVIGATION SYSTEM IN FLIGHT | 2012 |
|
RU2486472C1 |
INTEGRATED STRAPDOWN SYSTEM OF NAVIGATION OF AVERAGE ACCURACY FOR UNMANNED AERIAL VEHICLE | 2013 |
|
RU2539140C1 |
INDEPENDENT METHOD OF DETERMINING INITIAL ORIENTATION OF INSTRUMENT COORDINATE SYSTEM OF GIMBALLESS INERTIAL UNIT OF CONTROLLED OBJECT RELATIVE BASE COORDINATE SYSTEM | 2008 |
|
RU2386107C1 |
METHOD OF CALIBRATION OF SENSITIVE ELEMENTS OF STRAPDOWN INERTIAL NAVIGATION SYSTEM AND DEVICE FOR ITS IMPLEMENTATION | 2007 |
|
RU2334947C1 |
METHOD OF INCREASING GUIDANCE ACCURACY OF DEVELOPMENT STEPS FOR VARIOUS PURPOSES | 2010 |
|
RU2440557C9 |
MULTIFUNCTIONAL NAVIGATION SYSTEM FOR MOVING GROUND OBJECTS | 2015 |
|
RU2603821C2 |
CORRECTION METHOD OF STRAP-DOWN INERTIAL NAVIGATION SYSTEM | 2014 |
|
RU2564380C1 |
METHOD OF ESTIMATING ERRORS AND CONTROLLING RAW INFORMATION SENSORS IN GIMBALLESS INERTIAL NAVIGATION SYSTEM IN GROUND CONDITIONS AND APPARATUS THEREFOR | 2012 |
|
RU2537513C2 |
Authors
Dates
2007-10-27—Published
2005-11-15—Filed