METHOD FOR MONITORING OF PARAMETERS OF ROLL-STABILIZED GUIDED MISSILE, AND AUTOMATIC MONITORING SYSTEM FOR ITS REALIZATION Russian patent published in 2004 - IPC

Abstract RU 2243494 C2

FIELD: defense equipment, in particular, complex aids of monitoring of guided missiles.

SUBSTANCE: according to the invention, simulating values of command messages are assigned, they are modulated and converted to an electromagnetic radiation, than is fed to the input of the missile receiving channel, and the missile parameters are checked up. Simultaneously with the assignment of the simulating values of the command messages, a simulating signal of missile rolling is formed, and the signal is applied to the missile roll sensor. The current values of control commands are compared at the missile control actuator with the preliminarily assigned simulating values, and according to the results of the comparison, a conclusion is made on the conformity of the parameters under check with the assigned ones, the frequency of the missile rolling simulating signal is changed in the direct proportion to the missile flight simulating speed, and the missile guidance signal is modulated by a signal simulating the change of the missile attitude relative to the aiming point, in which realization is simplified at a high degree of accuracy of monitoring of the missile parameters. Two modifications of the automatic system of monitoring of the roll-stabilized missile are described.

EFFECT: simplified procedure at an enhanced accuracy.

4 cl, 4 dwg

Similar patents RU2243494C2

Title Year Author Number
METHOD FOR MONITORING OF PARAMETERS OF GUIDED MISSILE EQUIPMENT AND AUTOMATIC CHECK-OUT SYSTEM OR ITS REALIZATION 2005
  • Dudka Vjacheslav Dmitrievich
  • Zemlevskij Valerij Nikolaevich
  • Nazarov Jurij Mikhajlovich
RU2289781C1
PARAMETER CONTROL METHOD OF GUIDED MISSILE ROTATING ABOUT ANGLE OF ROLL, AND AUTOMATED CONTROL SYSTEM FOR ITS IMPLEMENTATION 2010
  • Dronov Evgenij Anatol'Evich
  • Boev Vladislav Il'Ich
  • Filisov Aleksandr Dmitrievich
  • Glazkov Konstantin Mikhajlovich
  • Omarbekov Boris Ramazanovich
  • Zemlevskij Valerij Nikolaevich
RU2438098C1
METHOD FOR MONITORING OF GUIDED MISSILE PARAMETERS AND AUTOMATED SYSTEM OF MONITORING OF GUIDED MISSILE PARAMETERS FOR ITS REALIZATION 2006
  • Stepanichev Igor' Veniaminovich
  • Ponjatskij Valerij Mariafovich
  • Chukanov Mikhail Nikolaevich
  • Matveev Ehduard L'Vovich
RU2316719C1
METHOD FOR FORMATION OF CONTROL COMMANDS ON ROLL-STABILIZED ROCKET, AND CONTROL SYSTEM OF ROLL-STABILIZED ROCKET 2004
  • Dudka Vjacheslav Dmitrievich
  • Zemlevskij Valerij Nikolaevich
  • Morozov Vladimir Ivanovich
  • Nazarov Jurij Mikhajlovich
RU2280226C1
METHOD FOR FORMATION OF CONTROL COMMANDS ON SPIN-STABILIZED ROCKET, ROCKET CONTROL SYSTEM, METHOD FOR FORMATION OF LINEARIZED SIGNAL AND SIGNAL LINEARIZER FOR ITS REALIZATION 2004
  • Dudka Vjacheslav Dmitrievich
  • Nazarov Jurij Mikhajlovich
  • Zemlevskij Valerij Nikolaevich
  • Morozov Vladimir Ivanovich
RU2282129C1
METHOD OF GENERATING CONTROL COMMANDS ON ROCKET ROTATING ON BANKING ANGLE, ROCKET CONTROL SYSTEM, METHOD OF MEASURING BANKING ANGLE ON ROCKET, GYROSCOPIC DEVICE FOR MEASURING BANKING ANGLE, METHOD OF GENERATING SINE AND COSINE SIGNALS ON ROCKET ROTATING ON BANKING ANGLE, AND SINE-COSINE ROCKET CONTROL SYSTEM GENERATOR 2012
  • Gusev Andrej Viktorovich
  • Kapustin Anatolij Sergeevich
  • Zapesochnyj Valerij Igor'Evich
  • Nazarov Jurij Mikhajlovich
  • Zemlevskij Valerij Nikolaevich
RU2514606C2
METHOD FOR ENTRY OF MISSILE INTO BEAM AREA AND COMPLEX OF MISSILE TELECONTROLLED IN BEAM FOR ITS REALIZATION (MODIFICATIONS) 2003
  • Zakharov L.G.
  • Zemlevskij V.N.
  • Kopylov Ju.D.
  • Kuznetsov Ju.M.
  • Zemlevskij O.V.
RU2257522C1
METHOD OF GENERATING CONTROL INSTRUCTIONS AT MISSILE SPINNING IN ROLL ANGLE AND SYSTEM TO THIS END, METHOD OF SELECTING SET PULSES AT MISSILE REVOLVING IN ROLL ANGLE AND DEVICE TO THIS EFFECT, AND METHOD OF DEFINING MISSILE ROLL ANGLE 2011
  • Gusev Andrej Viktorovich
  • Kuznetsov Vladimir Markovich
  • Nazarov Jurij Mikhajlovich
  • Zemlevskij Valerij Nikolaevich
  • Ovsenev Sergej Sergeevich
  • Tarasov Viktor Ivanovich
RU2473860C2
METHOD OF INTRODUCING ROCKETS INTO ZONE OF CONTROL, ROTATING ALONG ANGLE OF LIST, AND ROCKET SYSTEMS 2007
  • Morozov Vladimir Ivanovich
  • Nazarov Jurij Mikhajlovich
  • Zemlevskij Valerij Nikolaevich
RU2362107C2
METHOD OF GENERATING CONTROL INSTRUCTIONS FOR ROCKET ANGLE OF BANK, ROCKET CONTROL SYSTEM, METHOD OF CONVERTING IMPULSES OF ROCKET ROTATING ALONG ITS ANGLE OF BANK AND SINE-COSINE CONVERTER OF ROCKET CONTROL SYSTEM 2007
  • Stepanichev Igor' Veniaminovich
  • Zakharov Lev Grigor'Evich
  • Morozov Vladimir Ivanovich
  • Nazarov Jurij Mikhajlovich
  • Tjurin Vladimir Fedorovich
  • Zemlevskij Valerij Nikolaevich
RU2351875C2

RU 2 243 494 C2

Authors

Zakharov L.G.

Kopylov Ju.D.

Kuznetsov Ju.M.

Khandoshko L.P.

Zemlevskij O.V.

Dates

2004-12-27Published

2003-03-19Filed