METHOD FOR DETERMINING THE ORIENTATION OF AN OBJECT IN A STRAPDOWN INERTIAL NAVIGATION SYSTEM Russian patent published in 2023 - IPC G01C23/00 G01C21/20 

Abstract RU 2794283 C1

FIELD: instrumentation.

SUBSTANCE: invention can be used to create strapdown inertial navigation systems. The essence of the proposed method lies in projection of data acceleration of the object on the axis of the accompanying trihedron, which is sequentially carried out in two stages. At the first stage, n projections of the object acceleration data received from the accelerometers are formed onto the spatial axes of the auxiliary coordinate system, which coincides at the initial moment with the instrumental coordinate system and then remains motionless in the inertial space. At the second stage, after formation of n projections of the object acceleration data received from the accelerometers onto the coordinate axes of the auxiliary system, the average value is determined from n data projections onto the coordinate axes of the auxiliary system. Then the obtained data is transferred to the navigation calculator for designing the accompanying trihedron on the axis and using it to calculate navigation parameters, characterizing the orientation of the object in the strapdown inertial navigation system.

EFFECT: increase of accuracy and reliability of determining orientation of an object while expanding the arsenal of technical means.

1 cl, 2 dwg

Similar patents RU2794283C1

Title Year Author Number
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 AND DEVICE FOR EVALUATING NAVIGATION PARAMETERS OF CONTROLLED MOBILE OBJECTS 2003
  • Zajtsev S.A.
  • Kalinin A.I.
  • Makarchenko F.I.
  • Mezhiritskij E.L.
  • Rumjantsev G.N.
RU2241959C1
METHOD FOR DETERMINING NAVIGATIONAL PARAMETERS AND STRAPDOWN INERTIAL NAVIGATION SYSTEM FOR ITS IMPLEMENTATION 2016
  • Cherenkov Sergej Anatolevich
  • Lisin Aleksej Anatolevich
RU2634071C1
METHOD FOR CONSTRUCTION OF ASTROINERCIAL NAVIGATION SYSTEM 2016
  • Baburin Sergej Mikhajlovich
  • Silina Valentina Vileninovna
  • Danilov Oleg Yurevich
  • Sivokhina Tatyana Evgenevna
  • Cherenkov Sergej Anatolevich
RU2641515C2
INTEGRATED COMPLEX FOR NAVIGATION AND CONTROL OVER DEEP- SEA VESSELS 1997
  • Anuchin Oleg Nikolaevich
  • Gusinskij Valerij Zalmanovich
  • Emel'Jantsev Gennadij Ivanovich
RU2117253C1
SETTING OF MARINE STRAPDOWN INERTIAL NAVIGATION SYSTEM (SDINS) 2014
  • Andreev Aleksej Gur'Evich
  • Ermakov Vladimir Sergeevich
  • Mafter Mikhail Borisovich
RU2572651C1
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 OF COMPLEXING STRAPDOWN INERTIAL NAVIGATION SYSTEMS 2016
  • Baburin Sergej Mikhajlovich
  • Silina Valentina Vileninovna
  • Danilov Oleg Yurevich
  • Sivokhina Tatyana Evgenevna
  • Cherenkov Sergej Anatolevich
RU2634082C1
STRAPDOWN INTEGRATED NAVIGATION SYSTEM OF AVERAGE ACCURACY FOR MOBILE ONSHORE OBJECTS 2013
  • Salychev Oleg Stepanovich
RU2539131C1
NAVIGATION-PILOTING COMPLEX 2016
  • Baburin Sergej Mikhajlovich
  • Silina Valentina Vileninovna
  • Danilov Oleg Yurevich
  • Sivokhina Tatyana Evgenevna
  • Cherenkov Sergej Anatolevich
RU2634083C1

RU 2 794 283 C1

Authors

Ivanov Maksim Alekseevich

Cheremisenov Gennadij Viktorovich

Lyufanov Viktor Evgenevich

Kolbas Yurij Yurevich

Dates

2023-04-14Published

2022-08-11Filed