INDUCTION METHOD OF MEASUREMENT OF PARAMETERS OF MUTUAL POSITION OF MISSILE AND TARGET IN THE POINT OF IMPACT Russian patent published in 2006 - IPC G01C21/00 F41G9/00 

Abstract SU 1840312 A1

FIELD: complex tests of guided missile armament.

SUBSTANCE: the method is based on the principle of magnetometric measurements. The present values of the modi of signals induced in three mutually-perpendicular frame antennas of the receiving-measuring channels are measured on board the target, they correspond to the magnetic components of the rotating field produced on board the missile, and two present values of the phase difference of these signals in any two channels relative to the third channel taken as a reference one. The obtained information is transmitted to the recording point by means of a telemetric communication channel. The unknown values are calculated by formulas from the obtained values of these three modi and two phase differences.

EFFECT: enhanced precision of measurement and reduced overall dimensions of the equipment.

2 dwg

Similar patents SU1840312A1

Title Year Author Number
METHOD DETERMINING ORIENTATION OF OBJECTS IN SPACE, RANGE TO THEM AND BEARING, POSITION COORDINATES AND COMPONENTS OF VELOCITY VECTOR BY NAVIGATION RADIO SIGNALS OF SPACECRAFT OF SPACE RADIO NAVIGATION SYSTEMS 1998
  • Armizonov N.E.
  • Kozlov A.G.
  • Armizonov A.N.
  • Chmykh M.K.
RU2152625C1
METHOD FOR FORMATION OF STABILIZATION AND HOMING SIGNAL OF MOVABLE CARRIER AND ON-BOARD HOMING SYSTEM FOR ITS REALIZATION 2005
  • Berdichevskij German Efimovich
  • Shestun Andrej Nikolaevich
RU2303229C1
METHOD FOR INDEPENDENT INSTANTANEOUS DETERMINATION BY USERS OF CO-ORDINATES OF LOCATION, VELOCITY VECTOR COMPONENTS, ANGULAR ORIENTATION IN SPACE AND PHASE OF CARRIER PHASE OF RADIO SIGNALS OF GROUND RADIO BEACONS RETRANSMITTED BY SATELLITES 2004
  • Armizonov Aleksej Nikolaevich
RU2286584C2
METHOD FOR SHAPING CONTROL SIGNAL OF MISSILE DURING ORIENTATION AT MANOEUVRING TARGET 2009
  • Tolpegin Oleg Aleksandrovich
  • Emel'Janova Tat'Jana Jur'Evna
  • Sizova Anastasija Aleksandrovna
RU2419057C2
METHOD FOR SATELLITE CORRECTION OF GYROSCOPIC NAVIGATION SYSTEMS OF NAVAL OBJECTS 2008
  • Alekseev Sergej Petrovich
  • Reznichenko Vladimir Ivanovich
  • Maleev Pavel Ivanovich
  • Smirnov Mikhail Jur'Evich
RU2428659C2
METHOD FOR FORMATION OF TARGET POSITION IN EXPRESS MODE WITH LIMITED TIME OF FLYING UP OF ANTI-SHIP MISSILES WITH COMBINED HH, INCLUDING A SET OF KNOWN DEVICES FOR ITS IMPLEMENTATION AND VISUALIZATION 2019
  • Kozlov Olgerd Ivanovich
  • Marusenko Aleksandr Aleksandrovich
  • Prudnikov Evgenij Gennadevich
  • Fomichev Sergej Kapitonovich
  • Kharlanov Aleksej Ivanovich
  • Chernyavskij Nikolaj Vasilevich
  • Yadrevskij Evgenij Aleksandrovich
RU2726026C1
METHOD FOR SHAPING A MISSILE CONTROL SIGNAL WHEN GUIDING TO A MANEUVERING TARGET 2017
  • Lemeshonok Tatyana Yurevna
  • Tolpegin Oleg Aleksandrovich
RU2684432C2
METHOD OF CONTROLLING AND STABILISING MOBILE CARRIER, INTEGRATED SYSTEM, DEVICE FOR TURNING ANTENNA REFLECTOR IN TWO MUTUALLY-PERPENDICULAR PLANES AND DEVICE FOR ACTUATING DIFFERENTIAL AERODYNAMIC CONTROLLERS FOR REALISING SAID METHOD 2009
  • Berdichevskij German Efimovich
  • Blinov Valerij Anatol'Evich
  • Vorob'Ev Jurij Aleksandrovich
  • Shestun Andrej Nikolaevich
RU2423658C2
METHOD OF AUTONOMOUS ESTIMATION OF ORBIT CHANGES OF SIGHTED SPACECRAFT 2015
  • Kuznetsov Vladislav Ivanovich
  • Danilova Tamara Valentinovna
  • Arkhipova Marina Aleksandrovna
RU2624408C2
METHOD OF TWO-CHANNEL ATTITUDE CONTROL OF OBJECTS WITH SIX DEGREES OF FREEDOM OF SPATIAL MOTION 2016
  • Pavlov Viktor Andreevich
RU2629922C1

SU 1 840 312 A1

Authors

Tsyplakov Vladislav Vasil'Evich

Dates

2006-09-10Published

1966-04-05Filed