System for controlling and independently firing multiple missiles of different types
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F41F-030/55
F41F-030/77
F41F-030/52
출원번호
US-0014344
(1998-01-27)
발명자
/ 주소
Ivy Robert Leon
Goetz George Henry
Preston Timothy John
출원인 / 주소
Lockheed Martin Corp.
대리인 / 주소
Meise
인용정보
피인용 횟수 :
9인용 특허 :
4
초록▼
A launch system for plural missiles of different types includes plural launch locations, each adapted for receiving a canisterized missile having a standardized connector, which is coded to indicate the missile type contained within the canister. The system includes an individual fire control unit f
A launch system for plural missiles of different types includes plural launch locations, each adapted for receiving a canisterized missile having a standardized connector, which is coded to indicate the missile type contained within the canister. The system includes an individual fire control unit for each launch location or cell, and power supplies which are available to groups of such cells. An local-area network (LAN), such as Ethernet, interconnects the power supplies, the fire control units, and a central launch control system. Each fire control unit includes a processor for determining the missile type with which it is associated, and an interface card for each different missile type which may be used. The fire control units respond to commands from the central launch control system by interpreting the commands into a parallel form understandable by the missile interface cards. The missile interface cards transform the parallel data into serial data in a format suitable to the missile type being handled in the cell. Ancillary commands, such as launch hatch position and power-supply ON-OFF commands, are carried over the LAN.
대표청구항▼
[ What is claimed is:] [1.] A missile launching arrangement which is capable of launching a plurality of missile types, each of said missiles being loaded into a canister which has a standardized canister connector, which standardized canister connector includes pins which are jumpered in a manner w
[ What is claimed is:] [1.] A missile launching arrangement which is capable of launching a plurality of missile types, each of said missiles being loaded into a canister which has a standardized canister connector, which standardized canister connector includes pins which are jumpered in a manner which provides coding information identifying the type of missile within the canister, and also includes pins which provide a path for the flow of signals between the missile in the canister and the outside world, said missile launching arrangement comprising:a launch control system for maintaining an inventory of multiple missile types, and which, in response to external commands from a weapons control system, generates commands which identify the type of missile to be launched, and which also generates missile launch preparation commands and missile launch commands;a plurality of missile launch locations, each of which is capable of holding one of said missile canisters;a power supply module associated with at least one of said missile launch locations so that each of said missile launch locations has assigned to it at least one of said power supply modules, each of said power supply modules including a plurality of switchable voltage sources;a fire control unit associated with each one of said missile launch locations, each of said fire control units including an electronics module and a relay module, said electronics module and said relay module being connected by continuous electrically conductive paths to said standardized canister connector of that one of said canisters associated with the particular one of said missile launch locations with which said fire control unit is associated, said electronics module of said fire control unit also being connected to said launch control system and to the associated one of said relay modules, and each one of said relay modules also being connected to each of said switchable voltage sources of that one of said power supply modules associated with said associated one of said missile launch locations, for coupling the voltages of a selected set of said switchable voltage sources, which set may include only one switchable voltage source, to said standardized canister connector of that one of said missile canisters located in said associated one of said missile launch locations, each one of said electronics modules including a memory arrangement preloaded with information relating to a plurality of individual types of missiles, said electronics module being for performing a comparison of said coding of that one of said standardized canister connectors associated with that one of said missile canisters associated with said associated missile launch location, for identifying the type of missile contained therein, and for communicating said type of missile so identified to said launch control unit, each one of said fire control units also responding to arming and firing commands from said launch control unit directed to the one of said fire control units by producing, with the aid of that preprogrammed memory associated with its electronics module, a sequence of corresponding arming and firing commands appropriate to the particular missile type identified by the coding of said standardized canister connector, and for coupling said corresponding arming and firing commands to said standardized canister connector of that one of said canisters associated with the associated missile launch location.
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이 특허에 인용된 특허 (4)
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Sano Frank M. (Wayne NJ) Golden Edward J. (Sussex NJ) Sliwa Robert A. (Woodcliff Lake NJ), Weapon firing system including weapon interrogation means and stray voltage testing means.
Nelson, Steven; Carvalho, Joe; Diamond, Michael N., Methods and systems for defining addresses for pyrotechnic devices networked in an electronic ordnance system.
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