COMPENSATION OF QUADRATURED ERROR IN THE AUTO-OSCILLATION MICROMECHANICAL GYROSCOPE
Journal Title: Електроніка та системи управління - Year 2018, Vol 4, Issue 58
Abstract
In this paper, attention was paid to the analysis of the micromechanical sensor unit of the inertial navigation system as the main component of an unmanned aerial vehicle, as well as to improve the technical characteristics. This type of sensor is characterized by large instrumental errors and low sensitivity. In order to increase the sensitivity of a micromechanical gyroscope, the article proposes using resonant oscillation modes, which “enliven” its inertial mass. And in order to reduce the quadrature error of the gyroscope, which is one of the main obstacles to achieving its accuracy, it was proposed to reduce the level of these interferences not only using the synchronous detector, but also in front of it. A scheme is proposed that provides compensation for quadrature interference not by the mechanical moment generation contour, but by the output voltage channel. Since such a scheme does not affect the mechanical quadrature oscillations of the inertial mass, this effect can be interpreted as a self-oscillation mode, which increases the sensitivity of the secondary contour of the micromechanical gyroscope.
Authors and Affiliations
Мykola Filyashkin, Oleg Cherniai
COMPARISON OF BRIEF AND ORB BINARY DESCRIPTORS
A great deal of features detectors and descriptors are proposed nowadays for various computer vision applications. The task of image processing which is invariant to all weather conditions (such as rain, fog, smoke, unfa...
WIRELESS SOLAR POWER PLANT MONITORING SYSTEM
Monitoring systems are the most important part of modern solar power stations. Article contains the description of the existing monitoring systems, and their shortcomings are given. It is shown that as an alternative way...
CONCEPTUAL DESIGN OF SOLAR UNMANNED AERIAL VEHICLE
In this paper, emphasis was placed on the fact that a solar unmanned aerial vehicle, should be used in the context of certain missions, taking into account this, the general structure of the aircraft's internal systems w...
METHODS FOR IMPROVING THE DATA RELIABILITY IN INFORMATION AND CONTROL SYSTEMS
The paper deals with the questions of analysis and estimation the information reservation validity increase in information-control systems. A device for parallel-serial information reservation has been developed to incre...
ROBUST UAV CONTROL SYSTEM WITH REDUNDANT NONORTHOGONAL MEASURING INSTRUMENT
The paper deals with synthesis of robust system assigned for operation on unmanned aerial vehicles. A feature of the system lies in using nonorthoginal measuring instrument. Synthesis of the controller was carried out by...