METHOD AND EVALUATION SYSTEM OF IMPACT ZONE OF COMBAT LOAD LAUNCHED FROM AIRCRAFT Russian patent published in 2013 - IPC F41G7/00 

Abstract RU 2473861 C2

FIELD: instrument making.

SUBSTANCE: for evaluation of impact zone of ballistic or intelligent (automatically controlled) load of aircraft the system includes processing unit, collecting device of initial data or signals that indicate aircraft flight conditions at load release; and processing means that includes multiple neural networks for evaluation of target point of load killing. Note that processing unit additionally includes collecting device of secondary data or signals that indicate specified conditions of target killing, processing device can define polygonal zone of impact as functions from initial and secondary data or signals, and processing means includes multiple first neural networks made with the possibility of calculating coordinates of impact zone central point and specified quantity of impact zone tops.

EFFECT: extension of functional capabilities of intelligent load control.

15 cl, 7 dwg

Similar patents RU2473861C2

Title Year Author Number
MODULE-TYPE AIRCRAFT SIMULATOR 2004
  • Demchenko O.F.
  • Popovich K.F.
  • Pjaternev S.V.
  • Shkolin V.P.
  • Gurtovoj A.I.
  • Gabreljan A.A.
  • Pasekunov I.V.
  • Sorokin V.F.
  • Fedotov G.A.
  • Kodola V.G.
RU2247430C1
AIR SIMULATOR 2003
  • Baranov Nikolaj Alekseevich
  • Belotserkovskij Andrej Sergeevich
  • Kanevskij Mikhail Igorevich
  • Pasekunov Igor' Vladimirovich
RU2324982C2
METHOD FOR RECOGNIZING TYPICAL COMPOSITION OF A CLUSTERED AIR TARGET OF VARIOUS CLASSES UNDER VARIOUS CONDITIONS OF THEIR FLIGHT BASED ON KALMAN FILTERING AND A NEURAL NETWORK 2022
  • Bogdanov Aleksandr Viktorovich
  • Golubenko Valentin Aleksandrovich
  • Korotkov Sergej Sergeevich
  • Maksimovich Sergej Viktorovich
  • Petrov Sergej Gennadevich
  • Pshenitsyn Andrej Aleksandrovich
  • Shepranov Vitalij Vladimirovich
  • Yakunina Gayane Razmikovna
RU2802653C1
METHOD FOR ALL-ANGLE RECOGNITION IN RADAR STATION OF TYPICAL COMPOSITION OF GROUP AIR TARGET UNDER VARIOUS FLIGHT CONDITIONS AND INFLUENCE OF SPEED-CONTUSION INTERFERENCE BASED ON KALMAN FILTERING AND NEURAL NETWORK 2023
  • Bogdanov Aleksandr Viktorovich
  • Golubenko Valentin Aleksandrovich
  • Zakomoldin Denis Viktorovich
  • Korotkov Sergej Sergeevich
  • Maksimovich Sergej Viktorovich
  • Mironovich Sergej Yakovlevich
  • Petrov Sergej Gennadevich
  • Shepranov Vladimir Vitalevich
  • Yurin Grigorij Anatolevich
RU2816189C1
SYSTEM AND METHOD FOR DETECTING ERRONEOUS PRESSURE MEASUREMENTS IN AIR SIGNAL SYSTEM WITH NON-PROTRUDING PRESSURE RECEIVERS USING PRESSURE DIAGRAMS BETWEEN ADJACENT PRESSURE SAMPLING HOLES 2019
  • Jayakumar, M
  • Finitha, Kc
  • Remesh, N
  • Vidya, Sb
  • Shashi, Krishna
  • Jayanta, Dhaoya
  • Abdul Samad, Ak
  • Ravikumar, C
  • Shyam Mohan, N
RU2771090C1
SIMULATION METHOD ON FLIGHT TEST BENCH OF AIRCRAFT PENETRATION INTO VORTEX TRACE 2018
  • Animitsa Oleg Vladimirovich
  • Bobylev Anatolij Vladimirovich
  • Desyatnik Pavel Anatolevich
  • Zajchik Larisa Evgenevna
  • Kuzmin Petr Viktorovich
  • Sviridenko Yurij Nikolaevich
  • Suprunenko Stanislav Nikolaevich
RU2701062C1
SYSTEM AND METHOD FOR POSITIONING AND CONTROLLING THE AIRCRAFT AS IT MOVES ALONG THE TAXIWAY 2019
  • Staudinger, Tajler K.
  • Kellakhan, Kevin S.
  • Cheng, Ajzak
  • Dejm, Stefan
  • Evans, Nik S.
  • Jorgensen, Zakari D.
  • Kalin, Dzhoshua
  • Muir, Erik R.
RU2753004C2
IMAGE DECODING METHOD 2015
  • Akinina Natalya Viktorovna
  • Soldatenko Ilya Sergeevich
  • Semenova Irina Aleksandrovna
  • Shishkova Tatyana Evgenevna
RU2610283C1
AUTOMATIC REFUELING SYSTEM OF AN UNMANNED AERIAL VEHICLE 2020
  • Telnykh Aleksandr Aleksandrovich
  • Stasenko Sergej Viktorovich
  • Nujdel Irina Vladimirovna
  • Shemagina Olga Vladimirovna
RU2757400C1
VIBRATION DIAGNOSTIC METHOD OF GAS TURBINE ENGINE 2015
  • Tyapkin Sergej Aleksandrovich
RU2688340C2

RU 2 473 861 C2

Authors

Trankero Bruno

Dzhura Al'Berto

Konverso Stefanija

Dates

2013-01-27Published

2008-04-09Filed