DEVICE AND METHOD TO MEASURE GRAVITATION Russian patent published in 2000 - IPC

Abstract RU 2144686 C1

FIELD: geology, geophysical prospecting, high-precision navigation. SUBSTANCE: measurements are taken with the aid of acceleration transmitter mounted on moving carrier, satellite navigation receiver and computer. In the interests of vector gravimetry there can be used several acceleration transmitters, satellite navigation receiver for complete measurement of inertial acceleration should determine orientation in addition to position. Computer to integrate measured complete acceleration with inertial acceleration to determine gravitation can be used separately (under off-line condition). Besides, digital filtration of measured accelerations is improved considerably as compared with "physically blind" filtration of low frequencies thanks to proper selection of coefficients of filter matched in optimum way to stochastic characteristics of gravitational field of the Earth. EFFECT: usage of simpler and less expensive accelerometer, realization of vector gravimetry, that is, determination of complete gravitation vector and provision for definition of thinner structures of gravitational field of the Earth by means of air and sea gravimetry. 11 cl, 4 dwg

Similar patents RU2144686C1

Title Year Author Number
ASTRO-INERTIAL NAVIGATION SYSTEM WITH CORRECTION FOR THE EARTH'S GRAVITATIONAL FIELD 2023
  • Polubekhin Aleksandr Ivanovich
  • Yurin Aleksandr Dmitrievich
  • Brajtkrajts Sergej Garrievich
  • Kiselev Sergej Konstantinovich
  • Golovanov Sergej Nikolaevich
  • Merkulova Irina Igorevna
  • Egorov Dmitrij Aleksandrovich
  • Shipulin Maksim Dmitrievich
  • Larionov Igor Olegovich
RU2820600C1
ASTRONOMICAL NAVIGATION SYSTEM 2014
  • Bolotnov Sergej Albertovich
  • Brajtkrajts Sergej Garrievich
  • Gerasimchuk Yurij Nikolaevich
  • Ilin Vladimir Konstantinovich
  • Kayutin Ivan Sergeevich
  • Lyudomirskij Maksim Borisovich
  • Trubitsin Gennadij Vasilevich
  • Yamshchikov Nikolaj Evgenevich
RU2607197C2
INTEGRATED STRAPDOWN SYSTEM OF NAVIGATION OF AVERAGE ACCURACY FOR UNMANNED AERIAL VEHICLE 2013
  • Salychev Oleg Stepanovich
  • Grigor'Ev Viktor Evgen'Evich
  • Makarov Nikolaj Nikolaevich
RU2539140C1
ASTRONOMICAL NAVIGATION SYSTEM 2015
  • Brajtkrajts Sergej Garievich
  • Polubekhin Aleksandr Ivanovich
  • Ilin Evgenij Mikhajlovich
  • Tsygankov Viktor Yurevich
  • Trubitsin Gennadij Vasilevich
  • Mikaelyan Samvel Vartanovich
RU2592715C1
STRAPDOWN INTEGRATED NAVIGATION SYSTEM OF AVERAGE ACCURACY FOR MOBILE ONSHORE OBJECTS 2013
  • Salychev Oleg Stepanovich
RU2539131C1
AEROGRAVIMETRIC COMPLEX 1996
  • Poljakov Lev Grigor'Evich
  • Chesnokov Gennadij Ivanovich
  • Trubitsyn Gennadij Vasil'Evich
  • Gorchitsa Gennadij Ivanovich
RU2090911C1
METHOD AND SYSTEM FOR ADAPTING NAVIGATION SYSTEM 2015
  • Shtajnkhardt Niko
  • Zurek Daniel
RU2667667C2
METHOD OF DETERMINING SPATIAL COORDINATES OF MOBILE OBJECTS AND INTEGRATED NAVIGATION SYSTEM FOR REALISING SAID METHOD 2010
  • Krutskikh Andrej Aleksandrovich
RU2443978C1
INERTIAL-SATELLITE NAVIGATION SYSTEM WITH COMBINATION APPLICATION OF SATELLITE DATA 2007
  • Fomichev Aleksej Alekseevich
  • Kolchev Andrej Borisovich
  • Uspenskij Valerij Borisovich
  • Broslavets Jurij Jur'Evich
  • Schastlivets Kirill Jur'Evich
  • Larionov Pavel Valer'Evich
  • Pugachev Roman Vladimirovich
  • Vakhitov Timur Nazipovich
  • Kitaev Sergej Mikhajlovich
RU2334199C1
GRAVITY TRANSDUCER AND APPLICATION TO HYDROCARBON EXPLORATION 2013
  • Lisitsas Dzhordzh
  • Guj Syan
RU2608632C2

RU 2 144 686 C1

Authors

Gerd Bedekker

Frants Lajsmjuller

Karl Khans Nojmajer

Dates

2000-01-20Published

1995-08-30Filed