INTEGRATED COMPUTER CONTROL (KUAV)

General Description
Product Specifications
Gallery & Media
Point of Contact for further follow up
Others
Product Manufacturer
Hindustan Aeronautics Limited (HAL)
Designing/Manufacturing agency
Designed & Developed by SLRDC
Product Description

The ICC (Integrated Computer Control) of KUAV will perform the 
Guidance, Navigation, and Control (GNC) functions to ensure a safe and 
successful flight mission under the stated operating conditions. The ICC 
interfaced with various cockpit panels, IFCS sensors, utility systems, 
actuators and other Avionics LRU’s of the KUAV platform. It is real time 
dual redundant computer (GNC) based on 64 bit power Pc’s.

Product Specification
PARAMETERS
Dimension & Weight - 124 (W) X 193.5 (H) X 318 (L) & 12 Kg
Power supply - 28 V with power consumption of 160 W
Communication interface - MIL 1553 (one), ARINC 429 (20) for digital bus and RS 422 (18), RS 232(2), RS 486 (2), and Ethernet (4) for series interface
Self test - PBIT, CBIT, IBIT : 600 Pino
No of inputs /outputs - MIL-STD-461F for EMI/EMC | MIL-STD-704F for power supply | MIL-STD-810G for environment
Compliance - DO-254, DO-178 for firmware and software
Contact : prasenjit[at]hal-india[dot]co[dot]in