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DRDO Image Fusion Techniques for Electro-optical Systems

Image fusion is a subset of the more general field of data fusion. Image fusion combines multiple images of the same scene with complimentary or redundant information to generate a new composite image with better quality and more features. It can provide a better interpretation of the scene than each of the single sensor images can do. The objective is to reduce uncertainty and minimize redundant information in the multisensory output while maximizing information present in a scene. It has received significant attention in defense systems, medical imaging, robotics and industry, etc.

Image fusion system requires number of processes to convert two or more input images into a fused image. Images from the individual sensors are pre-processed (image enhancement) and aligned with one of the reference frames. The FOV compensation and spatial alignment is performed through image registration process.

Finally these images are fused, as per the fusion methods and fusion rules to generate the fused imagery. Figure shows the generic processing requirement for the generation of fused imagery to create the single output image from multiple image frames of individual sensors.

There are multiples steps required for image fusion which are as follows.

Mechanical alignment of imaging sensors: Sensors installed on a platform or as a part of surveillance suite, are to be aligned so that their optical axes are made parallel to each other

Image registration: This step is required to compensate different resolution, sensors’ FOV so that corresponding pixels of two/ more sensors are overlapped at same position. It is achieved by electronic processing method.

Image fusion: Once, registration is completed successfully, pixel level fusion algorithms are applied to make composite image from multiple imaging sources to enhance the information.

Image Fusion

Various Image fusion algorithms, i.e., weighted average, HPF, Waveletbased and Laplacian Pyramid-based image fusion have been designed, simulated and their performance and computation requirements have been analyzed. FPGA and DSP-based image fusion hardware have been developed. Image synchronization, Affine Transform and bilinear interpolationbased image registration algorithm, weighted average, HPF and LaplacianPyramid (LAP) based image fusion algorithms have been implemented in hardware. Image Registration and fusion of video from EO Sensors has been implemented in real time.

Figure 2 Shows the image fusion-based surveillance system developed at the laboratory.

Image Results

Figure 1 shows the image acquired from CCD Camera, thermal imager and fused image. The first image is colour CCD image showing smoke due to fire and a person walking behind smoke is captured by LWIR camera. The Fused image captures information from both the sensors. Fused image clearly conveys that there is fire as well as a person present in the scene. Multi-sensor image fusion has received significant attention in defense systems, geosciences, medical imaging, remote sensing, robotics, industrial engineering, etc. In defence, target detection, tracking and classification system identification, concealed weapon detection, battlefield monitoring, night pilot guidance, improved situational assessment/ awareness, improved robustness, can utilize fused imagery for better situational awareness.

Recently, Indian Railway has shown interest to install this system in front of train engine so that traffic signal and any animal/person/vehicle/object on track can be seen and output is shown in single composite image. It will reduce the accidents due to poor visibility and in night conditions. The developed techniques are being used in systems like Drivers Night Sight (DNS) for AFV, etc. being developed at the laboratory.

There could be following applications in near future.

Surveillance suite in which multiple monitor cannot be accommodated.

Transmission of multi-sensor suite information to command headquarter, which can be clubbed in single image/ video stream.

Single video can be archived instead of multiple videos to save storage.

It can reduce operator’s fatigue to monitor multiple displays.
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ISRO's two major facilities a Hypersonic Wind Tunnel and a Shock Tunnel which are the third-largest in terms of size and simulation capability in the world.

These facilities were indigenously designed, developed, and 'Made in India' with the support of Indian industries.
IMG_20200613_172952.jpg

+A few critical technologies.

The one-meter Hypersonic Wind Tunnel and one meter Shock Tunnel have been established with a wide spectrum of simulation capabilities in terms of Mach number, Reynolds number, and re-entry velocities.
IMG_20200613_173059.jpg

+The new facility would help aerodynamic characterization of advanced space transportation systems.

ISRO is planning to use them for its various programs like Reusable Launch Vehicles, Two Stage to Orbit, Air Breathing propulsion systems, and Human Space Flight Programme.
+
these facilities would also be used for military purposes like testing of hypersonic missiles, re-entry vehicles like MIRV, MaRV, etc in the future.
IMG_20200613_173154.jpg
 

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DRDO's 1.6 mJ Capacitor Bank that is used to power ARDE's two Railguns of 12 mm& 30 mm bore.

The capacitor bank is modular and is made up of 4 x 400 kJ modules.
Muzzle velocity of 1500 m/s was achieved for an 8 gm projectile.
550 m/s for 120 gm.
IMG_20200613_173401.jpg
 

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Development of New Weapon systems: Analysed the current and futuristic requirements of Missiles & Guided Weapon Systems with all stake holders, new projects have been taken up and being executed to further strengthen the arsenal of Armed Forces:

QRSAM ‐ Quick Reaction Surface to Air Missile flight tests are being conducted
Akash1S ‐ Surface to Air Missile with indigenous seeker has been successfully flight tested
Rudram II ‐ Air to Surface Missile with a range of upto 330km
Rudram III ‐ Air to Surface Missile with a range of upto 550km
SLCM ‐ Submarine launched Cruise Missile
Pralay ‐ Surface to Surface tactical Missile
High Power Electromagnetic Weapon for tactical applications
Liquid Fuel Ramjet (LFRJ) based supersonic target
Solid Fuel Ducted Ramjet (SFDR) based Missile for long range Air to Air application
MRSAM (Army) ‐ Medium Range Surface to Air Missile for Indian Army
Akash NG ‐ New Generation Surface to Air Missile with state‐of‐the‐art Seeker system
NGARM ‐ New Generation Air to Surface Anti Radiation Missile
Short and Medium range Naval Anti Ship Missiles
SANT ‐ Stand‐off Anti Tank Missile with MMW Seeker
VSHORAD ‐ Very Short Range Air Defence System
MPATGM ‐ Man Portable Anti Tank Guided Missile
LRSAM IAC ‐ Long Range Surface to Air Missile for Indigenous Aircraft Carrier
 

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Development of New Weapon systems: Analysed the current and futuristic requirements of Missiles & Guided Weapon Systems with all stake holders, new projects have been taken up and being executed to further strengthen the arsenal of Armed Forces:

QRSAM ‐ Quick Reaction Surface to Air Missile flight tests are being conducted
Akash1S ‐ Surface to Air Missile with indigenous seeker has been successfully flight tested
Rudram II ‐ Air to Surface Missile with a range of upto 330km
Rudram III ‐ Air to Surface Missile with a range of upto 550km
SLCM ‐ Submarine launched Cruise Missile
Pralay ‐ Surface to Surface tactical Missile
High Power Electromagnetic Weapon for tactical applications
Liquid Fuel Ramjet (LFRJ) based supersonic target
Solid Fuel Ducted Ramjet (SFDR) based Missile for long range Air to Air application
MRSAM (Army) ‐ Medium Range Surface to Air Missile for Indian Army
Akash NG ‐ New Generation Surface to Air Missile with state‐of‐the‐art Seeker system
NGARM ‐ New Generation Air to Surface Anti Radiation Missile
Short and Medium range Naval Anti Ship Missiles
SANT ‐ Stand‐off Anti Tank Missile with MMW Seeker
VSHORAD ‐ Very Short Range Air Defence System
MPATGM ‐ Man Portable Anti Tank Guided Missile
LRSAM IAC ‐ Long Range Surface to Air Missile for Indigenous Aircraft Carrier
LRSAM IAC= Barak-8ER?
 

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Fuel Air Explosive Mine Clearing System by d DRDO

Protected by a rocket on to d minefield using a tubular launcher frm a safe stand-off to create a safe lane fr vehicles.

It consists of :

Extendable probe
Switching unit(impact fuze)
Fuel canister wth central burster charge.
View attachment 49920
+
▫It carries fuel for aerosol formation
▫Grenade ejection unit consisting of ejectable HE filled grenades fr d detonation of aerosol
▫rocket motor fr achieving desired range
retarding tail unit wth parachute achieving desired terminal parameters; n
▫Electronic delay unit
Remove the rocket motor& parachute. Encase the whole setup in a case. Fire it from a arty with proximity fuse.
 

Karthi

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Maya AUV

MAYA AUV has a streamlined torpedo like body propelled by a single thruster. For vehicle maneuvering, two stern planes and a single stern rudder underneath the hull are used.

maya auv.jpg


Maya cruising underwater.jpg


Maya cruising underwater

Maya cruising on surface.jpg


Maya cruising on surface

Maya fitted with sensors.jpg


Maya fitted with sensors
 

Karthi

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aad1.jpg



L&T Universal Launcher

This is an all-electric, multi-role, modern launcher, designed for a payload of over 2000 kilos and mounted on a TATRA vehicle.
Key features:
Suitable for a range of containerised / canisterised missiles
Enables both vertical and inclined launch modes
Electro-mechanical outriggers with an auto-levelling feature, for complete stability
 

Karthi

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ssbs.PNG



DRDO Short Span Bridging System 5m

It is a mechanically launched bridging system of MLC-70 load class to bridge small gaps and canals. In addition to bridging the smaller gaps, this bridging system will be compatible with SARVATRA bridging system.

Salient Features:

Pick and place bridge over gap.

Quick construction with minimum crew.
 

Karthi

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AUV 150 is a modular shallow water AUV having five degrees of freedom.

Fully assembled AUV at Idukki Lake, Cochin.jpg


Fully assembled AUV at Idukki Lake.

3D view of modular AUV-1502.jpg


3D view of modular AUV-150.


Snapshot of deck on sagarnidhi, launching AUV-150.jpg


Snapshot of deck on sagarnidhi, launching AUV-150.



Navigation and Control of AUV 1502.jpg


Navigation and Control of AUV 150


The propulsion and associated control scheme of this AUV designed for thrusters mounted at appropriate locations to allow hovering of AUV at a particular depth while performing seabed mapping.


The AUV was powered by lithium polymer
battery pack residing inside a pressure hull. Navigation autonomy was achieved by using an integrated sensor framework consisting of INS, DVL and GPS.

Acoustic positioning of the AUV while submerged was established with USBL technology integrated with acoustic modem.


SONAR based collision detection was utilized for local path planning.
 

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