METHOD OF INCREASE OF RANGE OF ANGLES OF PRODUCT ROTATION WITH REFERENCE TO GYROSTABILISED PLATFORM INSTALLED ON PRODUCT IN GIMBALS Russian patent published in 2015 - IPC G01C21/24 

Abstract RU 2552857 C1

FIELD: instrument making.

SUBSTANCE: with reference to the gyrostabilised platform (GSP) installed on the product in gimbals the angles of rotation around longitudinal, transversal and vertical axes of the product are increased due to machine switching of the three-axis gimbals by signals from PC computer from the operating mode with "rocket" angles into the operating mode with "plane" angles and back to the pre-set (required) number of times by means of the rotation mechanism engine (RME) installed on the additional external frame of GSP gimbals. Note that the axis of rotation of the additional frame with reference to the aircraft (A) is installed collinearly to the aircraft vertical axis.

EFFECT: expansion of functional capabilities.

3 dwg

Similar patents RU2552857C1

Title Year Author Number
CARDAN SUSPENSION DEVICE FOR INCREASING ANGULAR RANGE OF ARTICLE ROTATION 2017
  • Makarchenko Fedor Ivanovich
  • Mezhiritskij Efim Leonidovich
  • Rumyantsev Gennadij Nikolaevich
  • Sapozhnikov Aleksandr Ilarievich
RU2654307C1
METHOD OF INCREASING GUIDANCE ACCURACY OF DEVELOPMENT STEPS FOR VARIOUS PURPOSES 2010
  • Makarchenko Fedor Ivanovich
  • Rumjantsev Gennadij Nikolaevich
RU2440557C9
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
COMBINED SYSTEM OF ORIENTATION AND NAVIGATION OF MOVING OBJECT 2020
  • Skripkin Aleksandr Aleksandrovich
RU2746236C1
INDEPENDENT METHOD OF DETERMINING INITIAL ORIENTATION OF INSTRUMENT COORDINATE SYSTEM OF GIMBALLESS INERTIAL UNIT OF CONTROLLED OBJECT RELATIVE BASE COORDINATE SYSTEM 2008
  • Makarchenko Fedor Ivanovich
  • Gusev Andrej Aleksandrovich
  • Makarchenko Oleg Fedorovich
RU2386107C1
METHOD FOR DETERMINING OBJECT ORIENTATION PARAMETERS USING SEMI-ANALYTICAL INERTIAL NAVIGATION SYSTEM WITH GEOGRAPHICAL ORIENTATION OF FOUR-AXIS GYROPLATFORM AXES 2022
  • Redkin Sergej Petrovich
RU2782334C1
METHOD FOR CALIBRATING DINAMICALLY ADJUSTABLE GYROSCOPE AS PART OF INERTIAL NAVIGATION SYSTEM 2020
  • Redkin Sergej Petrovich
  • Trebukhov Andrej Viktorovich
RU2741501C1
METHOD OF CALIBRATION OF SENSITIVE ELEMENTS OF STRAPDOWN INERTIAL NAVIGATION SYSTEM AND DEVICE FOR ITS IMPLEMENTATION 2007
  • Makarchenko Fedor Ivanovich
  • Kalinin Anatolij Ivanovich
  • Zajtsev Sergej Aleksandrovich
  • Rumjantsev Gennadij Nikolaevich
RU2334947C1
GYRO-STABILISED PAYLOAD STABILISATION SYSTEM OF AN UNMANNED AERIAL VEHICLE 2021
  • Florov Aleksej Vadimovich
  • Spiridonov Konstantin Vitalevich
  • Kalmykov Nikita Sergeevich
  • Voronkov Ilya Vladimirovich
  • Golubtsov Sergej Andreevich
  • Minyukov Kirill Ruslanovich
  • Maktaz Nikita Dmitrievich
  • Putyatin Pavel Valerevich
RU2762217C1
ORIENTATION SYSTEM 2003
  • Plotnikov P.K.
  • Musatov V.Ju.
  • Bol'Shakov A.A.
RU2239160C1

RU 2 552 857 C1

Authors

Makarchenko Oleg Fedorovich

Makarchenko Fedor Ivanovich

Nilov Aleksej Vladimirovich

Rumjantsev Gennadij Nikolaevich

Sukhov Sergej Vladimirovich

Dates

2015-06-10Published

2013-11-25Filed