CONSTRUCTION OF AN ADJUSTABLE AUTONOMOUS STRAPDOWN INERTIAL VERTICAL GYRO
Annotation
A variant of constructing a strapdown inertial vertical gyro with the use of correction for the indicated speed and barometric altitude is studied. Integration is performed on the basis of an extended Kalman filter for an aircraft of the airplane scheme. The pitch and roll angles are used as parameters of the local vertical direction. Mathematical modeling is carried out.
Keywords
Постоянный URL
Articles in current issue
- ADAPTIVE OBSERVER OF STATE VARIABLES OF A NONLINEAR NONSTATIONARY SYSTEM WITH UNKNOWN CONSTANT PARAMETERS
- CONSTRUCTION OF AN ADJUSTABLE AUTONOMOUS STRAPDOWN INERTIAL VERTICAL GYRO
- DETERMINING THE CLUSTER SIZE AND THE NUMBER OF REPLICAS OF HIGHLY LOADED INFORMATION SYSTEMS
- MODELING SHOCK-FRICTION INTERACTION OF THE FOOT WITH THE SUPPORTING SURFACE USING THE BASIS OF GENERALIZED HERMITE FUNCTIONS
- GRAPHICAL-ANALYTICAL METHOD FOR OPTIMAL SYNTHESIS OF PENDULUM CORRECTION CONTOUR OF VERTICAL GYROS
- DIGITAL OPTOELECTRONIC MEASURING DEVICE FOR MONITORING LARGE-SIZED SHELLS OF REVOLUTION
- METHOD FOR OVERALL CALCULATION OF AN INTEGRAL-FIELD MIRROR MODULE
- SPATIAL MICRO-SCANNING OF PLANE-PARALLEL GLASS PLATE SURFACE BY THE INTERFERENCE METHOD
- METHOD FOR DETECTING A SMALL AMOUNT OF OIL CONTAMINANTS IN A LIQUID USING LASER FLUORESCENCE TECHNOLOGY
- EXPERIMENTAL STUDIES OF A THERMOELECTRIC DEVICE FOR COOLING DISCRETE ELECTRIC RADIO ELEMENTS