RMI is a processor based indication module which gives indication to the pilot and co-pilot in Mi-17 IV helicopter regarding the position of rudder available to them at any point during the flight.
Solid State Digital Video Recorder (SSDVR) is designed for high data storage of video and audio. This recorder will receive the video data from the day/night camera through a video processing card and audio data.
The function of SSDVR is to use SSD (Solid State Drive) to record and play the HMOSP (Helicopter Multi-mission Optronic Stabilized Payload) video in the cockpit unit.
FPGA based SSDVR can be operated by Multi-function display located in cockpit to record video and sound, read video and sound, play, stop, rewind, forward, pause, event marker and back to last mark (in STOP mode or in PLAY mode).
The Front-end Electronics LRU is designed to process and store various sensor parameters from the SONAR. The signal will be processed using Zynq Ultrascale+MPSoC.
The Multichannel Front-end Electronics for SONAR consists of four cards namely power supply card, either two signal conditioning card or two pre-amplifier card and one controller card.
Mission Control Unit is designed to acquire various sensor signals located in the Torpedo. The acquired signals will be processed by the Artix-7 FPGA and the TMS320 processor.
Mission Control Unit (MCU) is a microcontroller and FPGA based real time interface module that consists of,
1. CPU card
2. Power Distribution Card
3. Mother Board
Instrumentation System relates to underwater decoys and more particularly to a device when placed in the underwater which also emits signals and navigates similar to those produced by a submarine.
The low power embedded processing system is realized by integrating the developed Xilinx Zynq Ultrascale+ FPGA 3U Rugged System Unit in a 4-Slot 3U VPX chassis. The form factor of the board is 3U VPX, and also 3U VPX Conduction cooled Gigabit Ethernet switch with 16 Gigabit ports with 9K jumbo frame support and L200 ruggedisation level is used to communicate within and external to the system.
Multichannel DAS is used to acquire hydrophone signals of frequency range 1Hz to 25kHz with 8 channels and maximum of 16 channels. The recording system has a delta-sigma A/D converter that provides digital antialias filtering and data to be stored in integrated Solid State Drive (SSD). The complete system power is controlled by microcontroller based power management unit and it is built around low power processor with various interfaces such as DDR, Flash, RTC, Ethernet, USB, RS232, SATA, and Sigma-Delta simultaneous ADC.
The Exciter/Receiver Module is Central Unit (CU) main RF section. The Exciter generates the timing and the TX drive signals for the radar system. The Receiver amplifies and down converts the received signal to IF frequency at 70MHz, and Bandwidth of 4MHz for IF sampling by the A/D. The Exciter/Receiver consists of four cards, i. Receiver Card ii. Synthesizer (PLL) Card iii. Combiner and TX Card iv. Logic Card
The UHF & VHF phase shifter is designed to detect the object by changing the phase.
UHF/VHF Shift unit is a receiver module which operates at VHF/UHF range frequencies.
The system developed and assembled in a 3U rack, which operates at DC voltage.
The system designed with 2 RF inputs and 4 IF outputs for both UHF/VHF Shift unit.
The X-Band DSERP hardware unit mainly consists of two boards which are signal processing board and AFE daughter board. The signal processor board contains Agilex 7 series FPGA and the other interfaces required for digital signal processing and AFE daughter board contains RF transceiver IC AFE7950 which has 4TX and 6RX for processing RF signals in the range of 600MHz to 12GHz.
Transmission Controller LRU is designed to measure and store the various sensor parameters located in transmission controller and combat vehicle.
The signal will be processed using Zynq SoC.
The 32-bit Multi core processor based transmission controller is designed to be Modular Card based system for easy maintenance. The transmission controller shall work on vehicle voltage of 24V Direct Current (DC). The transmission controller processes the inputs from various analog and digital sensors integrated in transmission and engine. The sensor signals shall be conditioned, Opto isolated and level translated by I/O card of the transmission controller.
Gear Selector Lever is used to shift the gears in the Combat Vehicle (Arjun Tank). The lever is provided with three positions: 1, 2 and A. The lever is also provided with four modes: Neutral mode, Driving mode, Reverse mode and Pivot mode. The reset button shall be pressed before shifting from one mode to another.
The Array Calibration Unit will operate between X-band to Ku-Band. This LRU is developed for measuring the gain and phase difference of the signal, and also used to calibrate the radar antenna.
The ACU will sample Low-IF signal and performs digital down conversion to create Baseband I/Q data. The Array Calibration Unit receives signals from array antennas with frequencies ranging from 10.95 GHz to 14.5 GHz and amplitudes ranging from -40 to -85dBm. This system includes a Transmitter Unit and a Receiver Unit, both includes a built-in PLL Source.
The LRU will transmit and receive the signal in W-Band.
These LRUs are designed to measure the density of the plasma particle.
The W-Band Trans-Receiver Subsystem consists of Transmitter Unit and Receiver Unit which operates at 75GHz to 110GHz frequency with 230VAC power supply.
The system designed with waveguide and assembled in 19”rack with WR-10 output ports.
The VRCMS is developed for monitoring gamma radioactive contamination of vehicles transiting in and out from a facility as well to detect the illicit movement of radiation source or special nuclear materials on or inside the vehicle. There are two self-contained, weather resistant gamma radiation detector pillars placed on either side of the roadway to be monitored.
The occupancy sensor installed on fixed pillar will detect the presence of vehicle at the range of 2 meters. The system’s fixed pillar is provided with battery, power supply, display and a system controller. The system is equipped with camera on both side of the fixed pillar for capturing image of vehicle in case of contamination.
Personal Radiation Dosimeter for Aerospace Applications (PERDAA) is designed to measure the nuclear radiation present inside the crew module placed in GAGANYAN (radiation level from 100µR/h to 1000R/h)
User in the field is then able to get information on radiation dose, dose rate, date, time, and alarms data by using RS-422 interface. PERDAA module can be connected to GSE (Ground Support Equipment) using RS-422 interface for retrieval of stored information and observation.
A unique rotary mechanism for retraction and deployment is due to the limited volume of the bay and the higher brake energy to be absorbed when landing at high speed. Landing gear systems were delivered and integrated into the SWIFT air frame. After successful taxi trials, the first flight of SWIFT was conducted with developed Landing Gear System.
The Pralay Missile Stabilisation Assembly is designed and manufactured to glide the missile to a low-altitude transition with a high-speed cruise trajectory, after controlling the ballistic trajectory for a portion of its flight.
The metallic components of the parachute are the ones that integrate the parachute with the pilot. This is a life-saving components for the pilot, which is useful in many difficult situations. The metallic components used in parachutes are exposed to rigorous testing so that they will not compromise on the safety parameters in real-time.
An explosive projectile, such as a mortar bomb, is fired from a mortar at low velocity, short range, and very fast ballistic paths. Point Detonating (PD) fuzes are mechanical in nature and are used by the current 81mm Mortar HE bomb. These fuzes use a primary explosive detonator that is sensitive to heat, friction, shock, and EMI/EMC.
The Flank Arrays were designed for passive surveillance, but if an active sonar ping is within the range of their frequency, they can also pick it up. For target strength estimates in the active situation, the other submarines can be treated as an oblate spheroid. This structure is positioned on both sides of the submarine and holds the SONAR sensors.
The High Energy Nd: Glass Disc Laser amplifiers utilise LAMA Module Structure Assemblies (LMSA) for the design, development, and characterization of specialised optical components to meet a variety of applications for High Energy Laser Systems and many other lasers and Synchrotron Radiation Sources.
The Optical Unit Assembly for GMD Mk III is a Gap Measuring Device that has been created to measure the distance between river or canal banks with an accuracy of 0.5 to 50 metres and 1 to 1.5 km. It can measure a minimum of 10 metres.
Die Block is a set of Powder Sintering dies used to condense uranium dioxide powder into high-density cylindrical pellets enclosed in thin-walled Zircaloy tubes; the ends are sealed by resistance welding. These die sets are extremely accurate, with cavity sizes manufactured at a 5-micron tolerance and less than 10-microns between each cavity.
Solenoid Mounting & Alignment Assembly is used in the 10 MeV, 5 kW TW Electron Linac, where it is used to adjust the solenoids mounted precisely in order to get the necessary combined magnetic field profile for the ARPF (Agriculture Radiation Processing Facility).
The FDSS Quad-Copter drone for low-altitude surveillance missions. It is designed for Operations in complex environments with rapid deployment within 3 minutes.
The drone weight is about 5kg and It can achieve maximum 40 minutes of flight time. It can transmit long range live video feed upto 30km, it is ideal for collecting immediate data from any mission-critical area. And it is enabled with 3-axis gimbal RGB camera, can perform for all operations autonomously without human involvement.
It can be utilized for traffic monitoring and safety surveillance operations
FDSS VTOL is specifically designed for High altitude inspection, surveillance, search and rescue operations.
This VTOL has a unique structural V-tail design so it reduces the over all weight and increases the flight performance.
The aerodynamic design and smooth surface ensures low air resistance and increase in flight time. We can operate the drone upto 80 minutes With the quick-detachable design, it easy to assemble and deploy the drone within 5 minutes and also It reduces the transportation barriers.
•AMRs are self-navigating robots employing advanced sensor and AI technology
• They offer dynamic adaptability and easily switch between tasks and environments.
• These robots can autonomously navigate, plan paths, and avoid obstacles
• AGVs are robotic vehicles guided by pre-defined paths or tracks .
• They excel in repetitive tasks within controlled environments.
• AGVs rely on infrastructure like magnetic strips or wires.
