METHOD OF INSPECTING ALIGNMENT OF GYROSTABILISED PLATFORM OF INERTIAL SYSTEM Russian patent published in 2015 - IPC G01C25/00 

Abstract RU 2541152 C1

FIELD: physics.

SUBSTANCE: method comprises initial alignment of a gyrostabilised platform; determining orientation of the coordinate system associated with the gyrostabilised platform relative to the local horizontal coordinate system associated with the Earth; calculating the result of independent determination of the azimuth of the gyrostabilised platform αη; determining the astronomical azimuth ACE of the control element of the gyrostabilised platform, the position of the normal to which coincides with the zero reading of an angle φ sensor; at the end of the initial alignment, measuring the angle φ of the gyrostabilised platform around the axis of a gimbal suspension and determining the gyrocompassing error ΔA: ΔA=αη-ACE-φ; alignment of the gyrostabilised platform is considered to have passed the inspection of the gyrocompassing error does not exceed an acceptable value.

EFFECT: high reliability of inspecting initial alignment of a gyrostabilised platform.

3 dwg

Similar patents RU2541152C1

Title Year Author Number
METHOD OF INITIAL ALIGNMENT OF INERTIAL NAVIGATIONAL SYSTEM 2002
  • Andreev A.G.
  • Ermakov V.S.
  • Severov L.A.
  • Maksimov A.G.
  • Jakushin S.M.
RU2215994C1
METHOD OF CONTROL OF GYRO-STABILISED PLATFORM 2011
  • Brovkin Aleksandr Grigor'Evich
  • Chekalin Vladimir Ivanovich
RU2491508C1
METHOD OF ADJUSTMENT OF AIRBORNE GRAVITY GRADIOMETER 1988
  • Soroka A.I.
  • Vasin M.G.
SU1517582A1
DEVICE FOR AUTOMATIC ALIGNMENT OF GYROSTABILIZED PLATFORM OF INERTIAL SYSTEM 1993
  • Aleksandrov K.S.
  • Bogdanov V.S.
  • Vozhik V.G.
  • Kedrov V.D.
  • Levi Ju.V.
  • Sabanina N.S.
  • Tsvintarnyj V.Ja.
  • Tsypkina G.Ja.
RU2062990C1
GRAVIMETRIC METHOD TO DEFINE DEVIATION OF PLUMB-LINE IN OCEAN ON MOBILE OBJECT 2007
  • Dobrotvorskij Aleksandr Nikolaevich
  • Denesjuk Evgenij Andreevich
  • Katenin Vladimir Aleksandrovich
  • Ivanov Boris Evgen'Evich
RU2348009C1
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 OF ADJUSTMENT OF AIRBORNE GRAVITY GRADIOMETER 1989
  • Vasin M.G.
  • Soroka A.I.
SU1823661A1
CONTROL SYSTEM OF UNMANNED AIRCRAFT WITH NAVIGATIONAL COMPLEX 1994
  • Nikol'Tsev V.A.
  • Vojnov E.A.
  • Podval'Nykh A.S.
  • Jakovlev V.N.
  • Simanovskij I.V.
  • Podoplekin Ju.F.
  • Korzhavin G.A.
  • Andrievskij V.R.
  • Jakobson A.B.
  • Tsvintarnyj V.Ja.
  • Efremov G.A.
  • Tsarev V.P.
  • Martynenko V.T.
RU2046736C1
AUTONOMOUS COMPLEX FOR CORRECTION OF INERTIAL SYSTEMS OF PLATFORM ORIENTATION AND NAVIGATION OF MOBILE OBJECTS 2022
  • Proskuryakov German Mikhajlovich
  • Pylskij Viktor Aleksandrovich
RU2826826C2
METHOD OF INCREASING GUIDANCE ACCURACY OF DEVELOPMENT STEPS FOR VARIOUS PURPOSES 2010
  • Makarchenko Fedor Ivanovich
  • Rumjantsev Gennadij Nikolaevich
RU2440557C9

RU 2 541 152 C1

Authors

Chekalin Vladimir Ivanovich

Kazakov Igor' Dmitrievich

Dates

2015-02-10Published

2013-10-03Filed