Missile interface unit

• US 5,096,139 A
• Filed: 08/16/1990
• Issued: 03/17/1992
• Est. Priority Date: 08/16/1990
• Status: Expired due to Term

• Current Assignee: Raytheon Company (Rtx Corporation)
• Original Assignee: Hughes Aircraft Company (Rtx Corporation)
• Inventors: Griggs, Darrin C., Humm, Larry A., Feld, Charles M.
• Primary Examiner(s): Sotomayor, John B.
• Application Number:
  US07/568,300
• Time in Patent Office: 579 Days
• Field of Search: 244/3.1, 244/3.15
• US Class Current: 244/3.1
• CPC Class Codes: F41G 7/30 Command link guidance systems homing F41G7/2206

Abstract

In a launcher control system (12), a missile interface unit (29) for controlling a ground launched active radar guided missile (GLA) which is modular in construction. The missile interface unit (29) provides target position information and control signals for test and launch of the GLA, and power for activating the GLA, as well as determining the status of the GLA. It employs a plurality of cards (56-70), each card having a specific function and being interconnected by a backplane bus system (55) which also couples the cards (56-70) to other components of the launcher control system (12).

Claims

1. A launcher control system, for controlling at least one airborne vehicle, comprising a) primary interface means for providing target position information and control signals for test and launch of said airborne vehicle, and b) means for supplying power for activating said airborne vehicle as well as determining the status of said airborne vehicle;

said primary interface means including a plurality of cards, each card for performing a specific function, and bus means for interconnecting said cards and for coupling said cards to other components of the launcher control system, said plurality of cards comprising;

a tactical control card for initializing the airborne vehicle for launch, for translating target and guidance information for transmission to the airborne vehicle after launch, for sequencing message traffic after launch, and for managing target information;

a hardware control card for testing and monitoring operation of said plurality of cards, a horizontal reference unit, and an instrumentation system, and for sequencing and formatting message traffic;

an analog-to-digital card for converting analog signals to digital signals for input to said tactical control card and hardware control card;

a memory card for storing executable code for said tactical control card and hardware control card;

a launcher bus controller card for translating tactical messages into a proper protocol and format for transferring the messages to the airborne vehicle through the launcher, and for receiving status information from the airborne vehicle;

an input/output card for managing communication between a launcher control unit and said primary interface means, said communication including status information from the launcher control system and guidance information to said airborne vehicle; and

an input/output interface card for managing communication between the primary interface means and a transmitter, for controlling an antenna coupled to the transmitter and for providing power to said launcher.

2. The launcher control system as recited in claim 1 used to control a plurality of airborne vehicles.

3. The launcher control system of claim 2 wherein said airborne vehicles are each a ground launched active radar guided missile.

4. The launcher control system as recited in claim 1 wherein each card of said plurality of cards is easily removable from the launcher control system and easily replaceable.