RU2000100556A - METHOD FOR SEMI-PASSIVE SELF-GUIDING OF AIR-TO-AIR AIRCRAFT CONTROLLED ROCKET WITH A RADAR SELF-GUIDING HEAD - Google Patents

METHOD FOR SEMI-PASSIVE SELF-GUIDING OF AIR-TO-AIR AIRCRAFT CONTROLLED ROCKET WITH A RADAR SELF-GUIDING HEAD

Info

Publication number
RU2000100556A
RU2000100556A RU2000100556/02A RU2000100556A RU2000100556A RU 2000100556 A RU2000100556 A RU 2000100556A RU 2000100556/02 A RU2000100556/02 A RU 2000100556/02A RU 2000100556 A RU2000100556 A RU 2000100556A RU 2000100556 A RU2000100556 A RU 2000100556A
Authority
RU
Russia
Prior art keywords
air
guiding
self
semi
radar
Prior art date
Application number
RU2000100556/02A
Other languages
Russian (ru)
Other versions
RU2181869C2 (en
Inventor
Владимир Иванович Павлов
Андрей Александрович Маштак
Дмитрий Валентинович Зайцев
Original Assignee
Тамбовский военный авиационный инженерный институт
Filing date
Publication date
Application filed by Тамбовский военный авиационный инженерный институт filed Critical Тамбовский военный авиационный инженерный институт
Priority to RU2000100556/02A priority Critical patent/RU2181869C2/en
Priority claimed from RU2000100556/02A external-priority patent/RU2181869C2/en
Publication of RU2000100556A publication Critical patent/RU2000100556A/en
Application granted granted Critical
Publication of RU2181869C2 publication Critical patent/RU2181869C2/en

Links

Claims (1)

Способ полупассивного самонаведения авиационной управляемой ракеты "воздух-воздух" с радиолокационной головкой самонаведения, отличающийся тем, что для наведения управляемой ракеты используют сигналы излучения помеховых станций цели, которые обрабатываются на борту ракеты к виду, пригодному для самонаведения.A semi-passive homing method for an air-to-air aviation guided missile with a homing radar, characterized in that the radiation from the jamming stations of the target, which are processed on board the missile to a homing mode, is used to guide the guided missile.
RU2000100556/02A 2000-01-10 2000-01-10 Method for semi-passive homing of air-to-air guided missiles with radar homing head RU2181869C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2000100556/02A RU2181869C2 (en) 2000-01-10 2000-01-10 Method for semi-passive homing of air-to-air guided missiles with radar homing head

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2000100556/02A RU2181869C2 (en) 2000-01-10 2000-01-10 Method for semi-passive homing of air-to-air guided missiles with radar homing head

Publications (2)

Publication Number Publication Date
RU2000100556A true RU2000100556A (en) 2001-10-27
RU2181869C2 RU2181869C2 (en) 2002-04-27

Family

ID=20229196

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2000100556/02A RU2181869C2 (en) 2000-01-10 2000-01-10 Method for semi-passive homing of air-to-air guided missiles with radar homing head

Country Status (1)

Country Link
RU (1) RU2181869C2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2468381C1 (en) * 2011-05-18 2012-11-27 Открытое акционерное общество "Государственное машиностроительное конструкторское бюро "Вымпел" им. И.И. Торопова" Method of striking target producing coherent interference with missiles fitted with active radar seekers
RU2586819C9 (en) * 2015-03-03 2016-08-20 Открытое акционерное общество "Государственное машиностроительное конструкторское бюро "Вымпел" имени И.И. Торопова" Method of striking target producing coherent interference with missiles fitted with active radar seekers

Similar Documents

Publication Publication Date Title
NO20025464L (en) Radar device for object self-protection
TW355204B (en) Method for offering a phantom target
WO2006137897A3 (en) Method and apparatus for improved determination of range and angle of arrival utilizing a two-tone cw radar
SE0004531D0 (en) Rocket weapon system and method of controlling a rocket weapon system
WO2004109251A3 (en) Back illumination method for counter measuring ir guided missiles
CA2064497A1 (en) Process to defend objects emitting an infrared radiation and droppable bodies to carry out the process
AU570778B2 (en) Weapon system and missile for the structural destruction of an aerial target by means of a focussed charge
RU2000100556A (en) METHOD FOR SEMI-PASSIVE SELF-GUIDING OF AIR-TO-AIR AIRCRAFT CONTROLLED ROCKET WITH A RADAR SELF-GUIDING HEAD
EP2051039A1 (en) Method and assembly for defending against ballistic missiles with the help of diverting missiles
DE60302281D1 (en) Weapon containing a rocket mounted on a stealth plane and weapon system containing a stealth plane and such a weapon
GR3005931T3 (en)
GB2004038A (en) Missile seeker head vectoring system
TNSN98162A1 (en) A TARGET REMOTE CONTROL AIRCRAFT FOR MILITARY SHOOTING TRAINING.
RU2255297C1 (en) Radio-controlled missile
JPH04208400A (en) Guidance system for guided flying body
WO2004107065A3 (en) Predetermined miss-distance homing missile
JPS6457096A (en) Method of controlling guidance of parent and child type guided missile
RU97119308A (en) METHOD FOR COMBINED CONTROL OF AIRCRAFT
GB202205046D0 (en) A hyper-acoustic missile powered by multiple successive electric-laser jet engines is used against enemy missiles and aircraft at present and in the future.
Smith Missile technology focuses on standoff capability.
RU2021132860A (en) Method for controlling the direction of radiation of a probing signal in the implementation of semi-passive homing of guided air-to-air missiles with a radar homing head
Lin Digital simulation of adaptive guidance and control system of a homing missile.
Kozicharow Manufacturer plans harpoon upgrades.
JPS53600A (en) Projectile guiding method
Wang The midcourse guidance technology for tactical surface-to-air missiles