METHOD FOR DETERMINING NOISES IN MEASUREMENT DATA OF SENSITIVE ELEMENTS OF INERTIAL NAVIGATION SYSTEMS Russian patent published in 2017 - IPC G06F17/17 

Abstract RU 2638782 C2

FIELD: physics.

SUBSTANCE: method comprises the stages of recording and processing the measurement data of each sensitive element of the inertial navigation system. At the first stage of processing the measurement data an array of information averaging intervals multiple of the data sampling cycle is formed. At the second stage of processing the set of Allan variation values corresponding to the averaging intervals of the inertial navigation system sensing element is determined as the square of the quadratic mean of relative two-sample deviation of the measurement data. At the third stage of processing the resulting set of Allan variation value is approximated by a polynomial with degrees of -2, -1, 0, +1, +2. The coefficients of the polynomial approximant are chosen by minimizing its total absolute discrepancy with the values of the Allan variation on a logarithmic scale.

EFFECT: simplifying the implementation procedure and increasing the reliability of the determination of noise components in the measurement data of inertial navigation system sensing elements.

3 cl, 1 dwg

Similar patents RU2638782C2

Title Year Author Number
METHOD OF DETERMINATION OF TEMPERATURE DEPENDENCES OF SCALING FACTORS, ZERO SHIFTS AND ARRAY OF ORIENTATION OF AXES OF SENSITIVITY OF LASER GYROSCOPES AND PENDULUM ACCELEROMETERS AS PART OF INERTIAL MEASURING UNIT AT BENCH TESTS 2014
  • Skopin Konstantin Aleksandrovich
  • Kolbas Jurij Jur'Evich
  • Zubov Andrej Georgievich
  • Eremin Leonid Vital'Evich
  • Ivanov Maksim Alekseevich
RU2566427C1
METHOD FOR DETERMINING THE ULTIMATE ACCURACY OF ESTIMATING MICROSEISMIC QUASI-STATIONARY NOISE BACKGROUND 2021
  • Abaturov Mikhail Anatolevich
RU2759974C1
METHOD FOR MEASURING ERRORS OF THE INITIAL ALIGNMENT OF AN INERTIAL NAVIGATION SYSTEM WITHOUT REFERENCE TO EXTERNAL LANDMARKS 2021
  • Kolbas Yurij Yurevich
  • Cheremisenov Gennadij Viktorovich
  • Ivanov Maksim Alekseevich
  • Lyufanov Viktor Evgenevich
RU2779274C1
METHOD FOR SPACECRAFT FLIGHT PATH CORRECTION AND DEVICE FOR ITS IMPLEMENTATION 2013
  • Meleshkov Gennadij Andreevich
RU2537818C1
COMPLEX METHOD OF AIRCRAFT NAVIGATION 2016
  • Zaets Viktor Fedorovich
  • Kulabukhov Vladimir Sergeevich
  • Kachanov Boris Olegovich
  • Tuktarev Nikolaj Alekseevich
  • Grishin Dmitrij Viktorovich
  • Akhmedova Sabina Kurbanovna
  • Perepelitsin Anton Vadimovich
RU2646957C1
METHOD FOR INTEGRATION OF STRAPDOWN INERTIAL NAVIGATION SYSTEMS 2019
  • Titlyanov Vladimir Aleksandrovich
  • Yakushev Artem Anatolevich
  • Timonov Anatolij Sergeevich
  • Eliseev Sergej Stanislavovich
  • Egoshin Konstantin Viktorovich
  • Mafter Mikhail Borisovich
  • Kosolapov Vladimir Grigorevich
  • Smirnov Mikhail Yurevich
  • Chernyavets Vladimir Vasilevich
RU2708901C1
METHOD FOR COMPENSATION OF ANGULAR VELOCITY SENSOR ZERO SIGNAL DRIFT SYSTEMATIC COMPONENT 2019
  • Kaplin Aleksandr Yurevich
  • Korotin Andrej Anatolevich
  • Stepanov Mikhail Georgievich
  • Yarmolich Aleksej Grigorevich
RU2695439C1
SMALL-SIZE ADAPTIVE ATTITUDE-AND-HEADING REFERENCE SYSTEM 2016
  • Zaets Viktor Fedorovich
  • Kulabukhov Vladimir Sergeevich
  • Kachanov Boris Olegovich
  • Tuktarev Nikolaj Alekseevich
  • Grishin Dmitrij Viktorovich
  • Akhmedova Sabina Kurbanovna
  • Perepelitsin Anton Vadimovich
RU2714144C2
METHOD FOR CALIBRATING ERRORS OF INERTIAL MEASURING UNIT BASED ON LASER GYROSCOPES USING A DYNAMIC BENCH 2021
  • Alyunov Pavel Vladimirovich
  • Veselov Aleksandr Dmitrievich
  • Sukhanov Sergej Valerevich
RU2803878C2
METHOD OF NAVIGATING SPACECRAFT BASED ON CELESTIAL PERIODIC RADIATION SOURCES 2011
  • Avramenko Arkadij Efimovich
RU2453813C1

RU 2 638 782 C2

Authors

Kutovoj Denis Alekseevich

Perepelkina Svetlana Yurevna

Fedotov Andrej Anatolevich

Dates

2017-12-15Published

2016-03-21Filed