AN/AYK-14
| AN/AYK-14(V) | |
|---|---|
| Weapons Systems Computer | |
| Status | In use |
| Manufacturing Info | |
| Manufacturer | Control Data Corporation |
| Introduced | 1976 |
| Production Period | 1976–Present |
| No. Produced | >10,000 |
| Specifications | |
| Operating Temperature | −54 °C (−65 °F) to 71 °C (160 °F) --> |
| Usage | |
| Used by Aircraft | |
| Used by Military | US Navy |
The AN/AYK-14(V) is a family of computers for use in military weapons systems.[1] It is a general-purpose 16-bit microprogrammed computer, designed in 1976 by Control Data Corporation Aerospace Division in Bloomington, Minnesota intended for airborne vehicles and missions.[2] Its modular design provides for common firmware and support software. It is still in use on Navy fleet aircraft including the F/A-18, and the AV-8B. The AN/AYK-14(V) family of systems is designed to meet military standard MIL-E-5400 (airborne) requirements.[3]
General information
The AYK-14(V) computer was designed for military weapons systems, capable of operating at altitudes up to 70,000 feet and in temperatures ranging from -54C to 71C.[2] A complete AN/AYK-14(V) computer system is composed of processor, memory and input/output (I/O) modules.[1] The 16-bit CPU is based on the AMD 2900 series chips, capable of running between 0.3 and 2.3 mega-instructions per second (MIPS).[2]
In accordance with the Joint Electronics Type Designation System (JETDS), the "AN/AYK-14" designation represents the 14th design of an Army-Navy airborne electronic device for armament fire control equipment. The JETDS system also now is used to name all Department of Defense electronic systems.
Applications
- Aircraft
- F-18 Hornet Central Mission Computers
- LAMPS MKIII Central Mission and ESM Processor
- EA-6B Prowler Electronic Warfare Computer
- E-2C Hawkeye Passive Detection System Computer
- AV-8B Harrier II Central Mission Computer
- Lockheed EP-3 Electronic Data Processor
- P-3C Orion ESM Processor
- F-14 Tomcat Avionics Improvement Program
- Special applications
- ALWT Torpedo Guidance Computer
- ACLS Landing System Processor
- DASS ASW Training Computer
- Firebrand Drone Guidance Computer
History
The AYK-14(V), designed in 1976, had an original unit price of $185,000.[2] By 1986, it was designated as the US Navy's Standard Airborne Computer.[2] In 1987, the computer was upgraded delivering twice the performance and eight times the memory.[2] Upgraded again in 1991, the operational speed was improved to 18 MIPS.[2] Over 10,000 units have been delivered.[2]
Technical description
The AN/AYK-14(V) series of systems are microprogrammed computers, intended for airborne vehicles and missions, but are also capable of shipboard and land use.[3]
General characteristics
The AN/AYK-14(V) is a general-purpose 16-bit computer capable of 675 thousand operations per second. Its modular design provides for common firmware and support software.[3]
System specifications and features
General Features
The AN/AYK-14(V) is designed to be physically and functionally modular. It can be expanded with plug-ins and additional enclosures. It's microprogrammed to emulate an extended AN/UYK-20. LSI components are used, and the system is packaged in ARINC Air Transport Rack (ATR) enclosures.
Central Processor
- Microprogrammed
- 2's complement arithmetic
- Executive and user states
- Two sets of 16-word by 16-bit general registers
- Two status registers
- Three-level interrupt system
- Addressing to 524,288 words
- Fixed and floating-point arithmetic
- 4-, 8-, 16-, and 32-bit operands
- 16-, and 32-bit instructions
- Direct, indirect, and indexed addressing
- Optional hardware floating-point module
- Loadable/readable 32-bit RTC clock, 1-MHz rate; 16-bit monitor clock, 10-KHz rate
- Built-in-test functions
- Bootstrap PROM memory
- Power failure shutdown/recovery
- I/O controller capability
- Chaining capability
- Control memory for each channel
- Up to 16 channels in various combinations
- Interface to support equipment
- Sample instruction times
- Shift 1.5 μsec
- Add, subtract 0.8
- Multiply 4.2
- Divide 8.4
- Basis: single GPM, core memory, overlapped access, interleaved addresses
Memory control and memory
- Core memory module (CMM), 32K words of 18 bits
- Semiconductor memory module (SMM), 32K words of 18 bits
- Interchangeable core and semiconductor memory modules
- CMM has 900-nanosecond cycle time and 350-nanosecond access time
- SMM has 400-nanosecond cycle time and 200-nanosecond access time
- Interleaved or non-interleaved addressing
- Read/write expandable memory (RXM), 4K x 18-bit RAM with optional 4K PROM
- Parity bit per byte
- Protect features
- Write protect
- Read protect
- Execute protect
- Block protect in paging system
- Memory controller with paging to 524,288 words
I/O Processor (optional)
- I/O controller capability
- Instruction subset compatible with central processor
- Microprogrammed
- Usable in conjunction with a central processor or as a stand-alone processor
- Real-time and system clocks
- 16-word by 16-bit general register set
- Addressing to 65,536-words
- Fixed point 16-bit arithmetic
- Interface to support equipment
Subsystems
Processor
The general processing control module (GPM) and the processor support module (PSM) make up a 16-bit central processor. for a general purpose computer. The extended arithmetic unit (EAU) is 32-bit floating-point hardware, controlled by the GPM. An input/output processor (IOP) can be added to increase processing throughput. It can function as an input/output controller (IOC) or as a single-module, 16-bit general purpose CPU.[3]
Memory
The memory subsystem includes two 32K-word with an 18-bit word length. The memory control module (MCM) provides the interface between the GPM and the memory modules. The read/write expandable memory module (RXM) is a 4K word module with an 18-bit word that serves as memory for the IOP.[3]
Input / Output
The AN/AYK-14(V) can support up to 16 I/O channels. A single chassis provides four to six I/O channels. XN-3 type enclosures can be added to expand the number of I/O channels.[3] I/O module types include:
- MIL-STD-1553A avionics serial multiplex bus
- NTDS (fast, slow, ANEW, and serial) MIL-STD-1397
- RS-232-C
- PROTEUS
Environmental requirements
The AN/AYK-14(V) family of systems is designed to meet MIL-E-5400 (airborne) requirements.[3]
See also
References
- ^ a b "AN/AYK-14 (V) Navy Standard Airborne Computer Overview Including P3I" (PDF). Control Data Corporation.
- ^ a b c d e f g h Hajdu, Frank, "Control Data AN/AYK-14(V)", Rhode Island Computer Museum, retrieved January 11, 2025
- ^ a b c d e f g "AN/AYK-14 (V) Navy Standard Airborne Computer Technical Description" (PDF). Control Data Corporation.