JPS5734468A - Missile - Google Patents

Missile

Info

Publication number
JPS5734468A
JPS5734468A JP11011380A JP11011380A JPS5734468A JP S5734468 A JPS5734468 A JP S5734468A JP 11011380 A JP11011380 A JP 11011380A JP 11011380 A JP11011380 A JP 11011380A JP S5734468 A JPS5734468 A JP S5734468A
Authority
JP
Japan
Prior art keywords
mirror
target
antenna
radio wave
reflected
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP11011380A
Other languages
Japanese (ja)
Inventor
Hideo Yamane
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP11011380A priority Critical patent/JPS5734468A/en
Publication of JPS5734468A publication Critical patent/JPS5734468A/en
Pending legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S3/00—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
    • G01S3/78—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using electromagnetic waves other than radio waves
    • G01S3/782—Systems for determining direction or deviation from predetermined direction
    • G01S3/785—Systems for determining direction or deviation from predetermined direction using adjustment of orientation of directivity characteristics of a detector or detector system to give a desired condition of signal derived from that detector or detector system
    • G01S3/786—Systems for determining direction or deviation from predetermined direction using adjustment of orientation of directivity characteristics of a detector or detector system to give a desired condition of signal derived from that detector or detector system the desired condition being maintained automatically
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/008—Combinations of different guidance systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2246—Active homing systems, i.e. comprising both a transmitter and a receiver
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2253—Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2273—Homing guidance systems characterised by the type of waves
    • F41G7/2286—Homing guidance systems characterised by the type of waves using radio waves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2273—Homing guidance systems characterised by the type of waves
    • F41G7/2293—Homing guidance systems characterised by the type of waves using electromagnetic waves other than radio waves

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Details Of Aerials (AREA)

Abstract

PURPOSE:To use both infrared rays and radio waves by forming a mirror surface of a secondary mirror in such a way that the radio waves pass the mirror surface but the infrared rays are reflected, and providing an antenna behind the secondary mirror. CONSTITUTION:The output of a transmitter 12 of the radio wave is transmitted to the antenna 10 via a duplexer 11. The radio wave is transmitted through the secondary mirror 2, and irradiated to a target from a primary mirror 1. The radio wave reflected by the target is received by the antenna 10 via the primary mirror 1. The signal received by the antenna 10 is subjected to the amplitude modulation in proportion to the error angle between the target and a tracking system. In response to said signal, a servo part 20 is controlled. As the missile approaches the target plane, the infrared ray irradiated from the target plane is focused by the primary mirror 1, reflected by the secondary mirror 2, and reaches a sensor 5 via a reticle 4. The servo part 20 is controlled by the error angle signal caused by the radio wave or the infrared ray based on the switching state of a switch 19.
JP11011380A 1980-08-11 1980-08-11 Missile Pending JPS5734468A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11011380A JPS5734468A (en) 1980-08-11 1980-08-11 Missile

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11011380A JPS5734468A (en) 1980-08-11 1980-08-11 Missile

Publications (1)

Publication Number Publication Date
JPS5734468A true JPS5734468A (en) 1982-02-24

Family

ID=14527365

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11011380A Pending JPS5734468A (en) 1980-08-11 1980-08-11 Missile

Country Status (1)

Country Link
JP (1) JPS5734468A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60216199A (en) * 1984-04-12 1985-10-29 三菱電機株式会社 Antiship guided missile

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60216199A (en) * 1984-04-12 1985-10-29 三菱電機株式会社 Antiship guided missile

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