METHOD FOR DETERMINING ERRORS IN BASIC CHARACTERISTICS OF INERTIAL MEASURING DEVICE UNIT Russian patent published in 2017 - IPC G01C25/00 

Abstract RU 2626288 C1

FIELD: measuring equipment.

SUBSTANCE: method consists in implementing rotations of the inertial measuring device unit comprising, at least, three similar inertial measuring devices with non-coplanar sensitivity axes, with subsequent recording and processing the measurement information. In the subsequent measurement information processing at the first stage, the recalculation of the measurement information is performed from the output code for each triple non-coplanar meters into the absolute value of the physical characteristic effecting the device, by using the mathematical error model parameters of the inertial measuring device unit. At the second measurement information processing stage, the error function is drawn, determining the total deviation of the physical characteristic value obtained by using the main characteristic values of the inertial measuring device unit according to the output code, from the reference value. At the third measurement information processing stage, the mathematical error model parameters of the inertial measuring device unit are specified by minimizing the obtained error function with the multi-parameter optimisation.

EFFECT: expanding the functionality through improving the accuracy of estimating the mathematical error model parameters of the inertial measuring device unit, simplifying and accelerating the estimating process of the mathematical error model parameters of the inertial measuring device unit, reducing the restrictions on the typical provisions and reversals of the inertial measuring device unit, allowing to assess the parameters of the mathematical error model in the reduced mobility of the inertial measuring device unit.

1 dwg

Similar patents RU2626288C1

Title Year Author Number
METHOD OF DETERMINING ERRORS OF AN INERTIAL UNIT OF SENSITIVE ELEMENTS ON A BIAXIAL ROTARY TABLE 2019
  • Fedotov Andrej Anatolevich
  • Perepelkina Svetlana Yurevna
RU2717566C1
METHOD TO CALIBRATE SENSITIVE ELEMENTS OF PLATFORM-FREE INERTIAL NAVIGATION SYSTEM IN FLIGHT 2012
  • Makarchenko Fedor Ivanovich
  • Mezhiritskij Efim Leonidovich
  • Rumjantsev Gennadij Nikolaevich
  • Shkoda Valerija Arshakovna
RU2486472C1
METHOD FOR CALIBRATION OF PLATFORM-FREE INERTIAL NAVIGATION SYSTEMS 2009
  • Andreev Aleksej Gur'Evich
  • Ermakov Vladimir Sergeevich
  • Nikolaev Stanislav Georgievich
  • Kolevatov Andrej Petrovich
RU2406973C2
METHOD OF DETERMINING NAVIGATION PARAMETERS OF OBJECT AND STRAPDOWN INERTIAL NAVIGATION SYSTEM FOR IMPLEMENTATION OF METHOD 2017
  • Cherenkov Sergej Anatolevich
  • Lisin Aleksej Anatolevich
  • Khudyakov Aleksandr Aleksandrovich
RU2661446C1
METHOD OF DEFINING ERRORS OF ORIENTATION AXLES OF LASER GYROSCOPES AND PENDULUM ACCELEROMETERS IN A STRAP DOWN INERTIAL NAVIGATION SYSTEM 2018
  • Zubov Andrej Georgievich
  • Kolbas Yurij Yurevich
RU2683144C1
METHOD TO SELECT VALID INFORMATION AND TO IDENTIFY FAILURES OF ACCELEROMETERS AND SENSORS OF ANGULAR SPEED AT FIVE METERS IN EACH TRACT IN PLATFORMLESS INERTIAL NAVIGATION SYSTEM OF AIRCRAFT 2014
  • Dishel' Valerij Davidovich
  • Trunov Jurij Vadimovich
  • Kazakov Sergej Vasil'Evich
  • Maslov Andrej Aleksandrovich
  • Timofeev Aleksandr Anatol'Evich
  • Polisadov Vladimir Valer'Evich
RU2568191C1
INERTIAL NAVIGATION COMPLEX FOR HIGH-SPEED MANOEUVRING OBJECT 2016
  • Khmelevskij Anatolij Sergeevich
  • Shchipitsyn Anatolij Georgievich
  • Lysov Aleksandr Nikolaevich
  • Kovalenko Valentin Vladimirovich
RU2657293C1
METHOD FOR DETERMINING PARAMETERS OF MODEL OF MEASUREMENT ERRORS OF ACCELEROMETERS OF INERTIAL NAVIGATION SYSTEM AS PER SATELLITE NAVIGATION MEASUREMENTS 2012
  • Dishel' Viktor Davidovich
  • Mezhiritskij Efim Leonidovich
  • Nemkevich Viktor Andreevich
  • Sapozhnikov Aleksandr Ilarievich
  • Sokolova Natal'Ja Viktorovna
  • Bykov Andrej Konstantinovich
  • Sulimov Viktor Grigor'Evich
RU2504734C1
METHOD AND DEVICE FOR CALIBRATION OF INERTIAL MEASUREMENT MODULES 2015
  • Shorin Vitalij Sergeevich
  • Nikishin Vladimir Borisovich
  • Sinev Andrej Ivanovich
  • Karpov Mikhail Nikolaevich
  • Safina Veronika Mudarisovna
  • Safina Ekaterina Mudarisovna
RU2602736C1
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

RU 2 626 288 C1

Authors

Kutovoj Valerij Matveevich

Kutovoj Denis Alekseevich

Perepelkina Svetlana Yurevna

Fedotov Andrej Anatolevich

Dates

2017-07-25Published

2016-03-21Filed