Unmanned Air Vehicle System.pdf

7/27/2019 Unmanned Air Vehicle System.pdf

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KALAKSHETRA EXIMN 33, Panch Shila Park

New Delhi 110 017 (India)

Phone: +91-9811368049 & 9311723801

E-Mail: [email protected] & [email protected]

Skype ID: kalakshetra.exim
mailto:[email protected]:[email protected]:[email protected]:[email protected]


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KALAKSHETRA EXIMNew Delhi (India)

Professional Audio & Broadcasting Equipment's, Systems,Solutions & Servicing

Tactical Solar Chargers

Tactical Security & Surveillance Products & Systems for Military,

Para-Military & Police

Solar Street Lights

Off/Grid Tie Solar Power Systems for Homes, Commercial &Industrial Settings

Solar Water Heating Products & Solutions

All Seasons - Solar AC, LED Lights, Solar Fans, Homes Light

Systems

Solar Panels, Inverters, Charge Controllers, Data-Loggers etc.

Aquaspring Spas Spring Hot Tubs, Swim Spas, Walk-in Tub andPipeless Swimming Pools filters using American Materials using

Acrylics & Digital Controls

Carbon Footprint Software & Consultancy


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KALAKSHETRA PARTNERSHIPS

Global Solar (USA) South East Asia including India but

excluding Pakistan, China, Japan, & North Korea

Bverih Defence Systems (Israel)

Netline (Israel) India

Urban Aeronautics, Ltd. (Israel)

Hefei Win Power Co. Ltd (China)

Renergy (Taiwan) India

HEFEI POSEIDON SOLAR PV PUMP CO. LTD (China)

Halospas (China) Umberto (Germany)

ComsTrac Limited (UK)

CONTROP Precision Technologies Ltd (Israel)


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KALAKSHETRA EXIM

In Partnership with

Bverih Defence Systems (Israel)


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Unmanned Air Vehicle System

Micro UAV & Aerostat


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UAV/Aerostat with Payloads & its Accessories


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Micro UAV & Aerostat

Provides reliable real time intelligencegathering in high quality. The System consists ofthe UAV, the payload carried by the UAV, the

ground controlling and data-link componentswhich is a very cost-effective and reliablesystem, can be deployed in very short time, thesystem operation is simple and the HumanMachine Interface (HMI) is user-friendly and is

enabled to be carried in a specially designedpack system


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APPLICATIONSMilitary & Non-Military Usage

Surveillance, Reconnaissance and Target Acquisition

Border and coastal surveillance

Intelligence Search and Rescue

Police and law enforcement

Traffic control

Mine theft control

VIP & VVIP Security

Protection of sensitive installations - Power Stations, Oil Refineries.TV broadcasting stations

Sporting & Public events

Television broadcasting

Training aid


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Types of UAV Available

Aerostat

Aetos 316

Unmanned Aerial Vehicle

Pegasus 250


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Aerostat Balloon SystemFeatures

360 Degree observation coverage.

Small sized. Trailer transportable.

Day and night surveillance capability.

Operational manoeuvrability enabling 15 Minutes deployment.

Specialized Helium filling station system to enable fast inflation.

Aerostat transportable at 80% Helium capacity to enable

minimal filling and launch time.

Extremely difficult to damage from any ground projectile.

Totally integrated with C4i systems. Sophisticated technological design to enable minimal training

hours for successful operation


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Aerostat Balloon SystemFeatures

Aerostat payload features

Sensor: 3 CCD digital processing & day camera / infra red thermal sensor

Stabilization: 3- axis gyro Stabilization & Structure: Military grade composite material

Weight: 3 KG

Elevation field of view: +8 to - 105 degrees & Azimuth field of view: 360 Degrees continuous

Diameter: 200 mm (Excluding cradle) - Height: 320 mm

Electrical input voltage: 12 Vdc

Signal format: PAL / NTSC, Lens: F1.6 - 2,9 : 20 X power zoom 42 - 84 mm + 5 X digital zoom

and Output signal: 1 Vp-p

Aerostat Features

Can be packed down to small storage crate (1x 0.5 x 1 Meter) & Deployable by 2 - 3

operators in 30 minutes (including payloads)

Once inflated, aerostat can be transported by small size trailer & Very low operating cost.

(Only 1,000 cubic feet, helium inflation)

Proven performance

Aerostat Specifications

Inflated length: 25 Feet & Inflated Width: 9.5 Feet

Payload capacity for maximum altitude 9 lb & Recommended operating altitude. 500 ft

Anti aircraft collision lighting system


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Micro UAV SystemFeatures

Real time IMINT & Autonomous Flight Electric propulsion for covert and silent flying

Hand launched and self recovery, no L&R equipment or facilities required

Simple to operate

Easy to assemble and disassemble & Full flight systems contained in backpack

Ability to fly silently below the cloud base

Operator needs no pilots license. System software designed for on site minimal

training

All the flight characteristics automatically adjusts to the operator commands to the

camera

In the event of lost communication- the UAV automatically returns back to the

launching zone

Patented wing design allows final approach for landing at minimum speed, enabling

safe landing with no need for landing gear nor parachute


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Performance

Endurance. 3 Hours (Unlimited changeover with additional UAV units) Mission radius: 10-15 Km

Speed - 18-45 Knots

Technical Data

Take off weight:- 5 KG

Payloads - Color CCD camera system, flir camera for night missions and low visibility day time

Construction - Composite material

Optic payload adapted to specific usage

Applications

Immediate real time intelligence for front line units and special forces operations

Fast reaction requirements. (Launch time 75 Sec)

Urban military and police operations

Covert monitoring & Border surveillance

Payload sensors adapted to all uses including monitoring of contaminated areas.(i.e.

Nuclear materials, Gases, Chemical)

Search and rescue and early monitoring of bush-fires (thermal cameras)

Micro UAV SystemFeatures


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Mission Capabilities

The Tactical UAV system is designed to perform a widevariety of surveillance, intelligence and battlefield supportmissions, in the tactical level.

Typical military missions are as follows: Battlefield surveillance

Target acquisition

Battlefield monitoring

Air strike control

Border and customs patrol. Payload sensors includingmonitoring of contaminated areas (i.e. Nuclear materials,gases, chemical)

Coast guard surveillance. Search and rescue Payloads available for detection of nuclear materials

Damage assessment

Police. Urban and Special Forces


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Civil applications

The System can also be used for civilian orcommercial application such as: Pollution control at ground sea and air

Natural disasters monitoring

Forest fire early warning monitoring and control offire fighting personnel and early detection ofcivilians in

the path of the fire. (Early detection thru thermalcamera payloads from 7,000 ft detecting firesearly).

Fishery and navigation control

General installations security

Gas pipelines and Oil rigs security

Mining operations


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Systems OperationDescription, Flight Modes & Human resources

The system is capable to perform continuous missions, 7 days a week, 24-hour a

day. The UAV standard endurance per mission (depends on the flight profile, the

winds, payload installed and other variables).

1 UAV and 2 control stations are required. While one UAV is in the air, the other

UAV is prepared for the next mission. When the first UAV battery reaches to its

bottom limit, the second UAV replaces it above the target, and the first UAV is

returned to the lunching site to be prepared for the next mission (the third is areserved unit).

The Pegasus 250 System can autonomously perform a pre-programmed flight

mission. In addition, the operator can change the mission during flight.

The system is operated by a crew of 2 persons, with the following tasks

assignments:

Mission Commander: The mission commander is responsible for the mission execution,

mission safety and the communication with external factors. The mission commander is

also in charge of hand launching.

Field Pilot: The field pilot operates the control station in all mission phases (ground

checks, mission planning, flight, navigation, etc.) and is also in charge of payload

operation, communication with the intelligence customer and images interpretation.


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Pegasus 250 UAV Description

Air Vehicle

The Pegasus 250 is a Back Packed Tactical Unmanned Air Vehicle. The air vehicle

consists of a fuselage, telescopic boom and tail assembly, high wing on a pylon and a

specially developed electric engine and avionic systems. The Pegasus 250 is equipped

with inflated landing gear (Patented). The Pegasus 250 carries the payload installed in

the nose of the fuselage.

Other sub-systems installed inside the fuselage are: Batteries

Avionics package including all flight sensors and servo actuators

Communication system, composed of uplink as well as downlink

Electro-optical payload

Electrical power supplyPerformances

The Pegasus 250 performances are as follows: (Performances Parameter Specification)

Stall speed. 18 kts & Cruise speed 50 kts

Rate of climb > 700 f/min & Service ceiling. 8,000 Ft

Endurance in cruise speed > 2.5 hrs & Glide rate (no wind) 1:25


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Auto pilot System

The Auto pilot controls all the Pegasus 250 capabilities. The Auto pilot is based on powerful

purpose built processors equipped with serial communication port, and 8 PWM ports (for

servo). It has a built in flash memory to handle the operating system as well as the

applications. The Auto pilot performs all traditional functions such as flight control, mission

control, payload operation and data link management.

In addition to the computing elements, the Auto pilot contains solid-state airspeed and

altitude sensors, and a Global Positioning System (GPS). The following paragraphs provide a

brief description of the Auto pilot main functions, interfaces and flight sensors.Auto pilot Main Functions

The Auto pilot main functions

Flight control & stabilization Controls and stabilizes the Pegasus 250 in the 3 axis

Mission control Enables pre-programmed autonomous navigation by GPS and in-flight reprogramming

Payload control Normal operating mode in rate and position for the gimbals

System logic Enables emergency landing sequence

Data-link managementHandling and arranging the down-link and up-link messages

Auto pilot Interfaces

The Auto pilot is provided with the following input/output interfaces:

Servo actuators 8 PDM (PWM) Ports

Data linkuplink, downlink, Serial port RS 232


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Aerial Data-link system

The data-link sub-system is responsible for the communication between the

ground stations and the UAV. The link between the ground stations and the UAV iscomposed of uplink channel through which the commands to the UAV and payload

are transmitted, and a downlink channel for video and telemetry data

transmission from the UAV to the ground stations. The data-link controller is a part

of the Auto pilot avionics and no additional control hardware or software is

required. The data-link controller handles all uplink and downlink messages. The

interfaces between the data-link components and the Auto pilot are accomplished

through especially developed ports.

The Pegasus 250 aerial data-link system is comprised of the following

subassemblies:

Video transmitter

Command & telemetry transceiver

Omni directional antennas: Telemetry Antenna & L Band Antenna


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MCS - Mission Control Station

The Mission Control Station (MCS) is state of the art, universal unit designed to

operate Mini UAV platforms. It's based on advanced real time software. The MCSprimary function is to control and monitor UAV operation and its payload. Other

functions are: mission planning, pre-flight and post-flight maintenance procedures

and more. The MCS is communicating with the UAV through the Ground Data

Terminal (GDT). It transmits commands to the UAV, and receives telemetry

information as well as real time video images.


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Aerostat in use with military in urban areas


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Real time screen display with capability to transmit to multiple

destinations, securely and simultaneously


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Portable ground station installed in Car


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Payload connection before


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Thermal payload, showing


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Securing area before entry of crowds for visit of Pope. Ensuring

security by construction workers


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Barbados. Cricket. World Cup. 2007


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Public event security monitoring. (USA)


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Aerostat transmitting live to television stations during football

game. Millions saved in Helicopter air time. Cutting of green

house gases and increased safety for spectators from helicopter

malfunction (Italy)


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Unloading from trailer before deployment.

Diamond mine theft & Security (Botswana - Africa )


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Documents

Unmanned Air Vehicle System.pdf