JPS6467597A - Missile - Google Patents

Missile

Info

Publication number
JPS6467597A
JPS6467597A JP22298187A JP22298187A JPS6467597A JP S6467597 A JPS6467597 A JP S6467597A JP 22298187 A JP22298187 A JP 22298187A JP 22298187 A JP22298187 A JP 22298187A JP S6467597 A JPS6467597 A JP S6467597A
Authority
JP
Japan
Prior art keywords
projectile
launcher
data
warship
program
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
JP22298187A
Other languages
Japanese (ja)
Inventor
Fumiaki Tominaga
Hiroshi Hibino
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 Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
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 Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP22298187A priority Critical patent/JPS6467597A/en
Publication of JPS6467597A publication Critical patent/JPS6467597A/en
Pending legal-status Critical Current

Links

Landscapes

  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

PURPOSE: To incorporate a projectile easily in a program by making the guide calculation, navigation calculation, and other programs and data required at a desired time during an interval after assembling before launching a projectile readable entirely or partially. CONSTITUTION: When a launcher is different such that a projectile 1 is launched, respectively, from an aircraft 01, a moving vehicle 02 and a warship 03 toward a target warship 04, the projectile 1 is launched, respectively, from an aircraft launcher 01', a ground launcher 02' or a warship launcher 03' after a program and a data are read in and a program of guide calculation, navigation calculation, sequence control, or the like, suitable for each launching requirements is executed. when a data is inputted to the projectile 1 from any one launcher and a data only at a required position is inputted at the time of launching, a bulky volume of data conventionally read into the body prior to assembling the projectile in order to deal with various situations can be reduced.
JP22298187A 1987-09-08 1987-09-08 Missile Pending JPS6467597A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP22298187A JPS6467597A (en) 1987-09-08 1987-09-08 Missile

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP22298187A JPS6467597A (en) 1987-09-08 1987-09-08 Missile

Publications (1)

Publication Number Publication Date
JPS6467597A true JPS6467597A (en) 1989-03-14

Family

ID=16790926

Family Applications (1)

Application Number Title Priority Date Filing Date
JP22298187A Pending JPS6467597A (en) 1987-09-08 1987-09-08 Missile

Country Status (1)

Country Link
JP (1) JPS6467597A (en)

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4660170A (en) * 1985-04-29 1987-04-21 General Dynamics, Pomona Division System for providing reprogramming data to an embedded processor

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4660170A (en) * 1985-04-29 1987-04-21 General Dynamics, Pomona Division System for providing reprogramming data to an embedded processor

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