FIELD: instrumentation engineering; inertial control systems for evaluating navigation parameters of controlled mobile objects.
SUBSTANCE: sensing element of platform-free control system is mounted on stage in gimbal suspension, stage is rotated relative to object at speed close to that of object but different in sign, measurements are made of parameters of translational and rotational motion of stage, angular position and of object body relative to stage, measurement data obtained are processed, and navigation parameters of object motion in inertial space are calculated. Inertial system device implementing this method has gimbal suspension accommodating stage that mounts three accelerometers and three angular velocity sensors; angle sensor and motor are mounted on gimbal suspension axle; stage is revolved by means of motor at speed approaching that of object under control but in opposite direction; sensing element signals are processed and parameters of object movement as well as its positioning are found by means of computer that sums up signals proportional to turn angles of stage relative to base system of coordinates and signal arriving from angle sensor mounted on stage suspension axle.
EFFECT: enhanced measurement accuracy.
5 cl, 2 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF CALIBRATION OF SENSITIVE ELEMENTS OF STRAPDOWN INERTIAL NAVIGATION SYSTEM AND DEVICE FOR ITS IMPLEMENTATION | 2007 |
|
RU2334947C1 |
METHOD OF EVALUATION OF NAVIGATION PARAMETERS OF OPERATED MOBILE OBJECTS AND RELATED DEVICE FOR IMPLEMENTATION THEREOF | 2007 |
|
RU2339002C1 |
INDEPENDENT METHOD OF DETERMINING INITIAL ORIENTATION OF INSTRUMENT COORDINATE SYSTEM OF GIMBALLESS INERTIAL UNIT OF CONTROLLED OBJECT RELATIVE BASE COORDINATE SYSTEM | 2008 |
|
RU2386107C1 |
METHOD TO CALIBRATE SENSITIVE ELEMENTS OF PLATFORM-FREE INERTIAL NAVIGATION SYSTEM IN FLIGHT | 2012 |
|
RU2486472C1 |
METHOD OF DETERMINING INITIAL POSITION OF INERTIA BLOCK WITH RESPECT TO BASE COORDINATE SYSTEM | 2004 |
|
RU2279635C2 |
METHOD OF INCREASING GUIDANCE ACCURACY OF DEVELOPMENT STEPS FOR VARIOUS PURPOSES | 2010 |
|
RU2440557C9 |
METHOD FOR DETERMINING PARAMETERS OF MODEL OF MEASUREMENT ERRORS OF ACCELEROMETERS OF DRIVEN INERTIAL NAVIGATION SYSTEM AS PER MEASUREMENTS OF REFERENCE INERTIAL NAVIGATION SYSTEM | 2012 |
|
RU2505785C1 |
METHOD OF DETERMINING THE ANGLES OF ORIENTATION OF AN AIRCRAFT ON VERTICAL TRAJECTORIES OF FLIGHT | 2017 |
|
RU2671291C1 |
INERTIAL MEASUREMENT MODULE | 2021 |
|
RU2761592C1 |
METHOD FOR DETERMINING PARAMETERS OF MODEL OF MEASUREMENT ERRORS OF ACCELEROMETERS OF INERTIAL NAVIGATION SYSTEM AS PER SATELLITE NAVIGATION MEASUREMENTS | 2012 |
|
RU2504734C1 |
Authors
Dates
2004-12-10—Published
2003-05-20—Filed