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KZO TUAV / FTS / 08.02.2006 / Chart 1 Observe copyright as per ISO 16016 KZO Tactical UAV System Overview

KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

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Page 1: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

KZO TUAV / FTS / 08.02.2006 / Chart 1Observe copyright as per ISO 16016

KZOTactical UAV System

Overview

Page 2: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

Airborne Systems, KZO Tactical UAV System

KZO TUAV / FTS / 08.02.2006 / Chart 2Observe copyright as per ISO 16016

Content

� System Elements� Air Vehicle� Ground Control Station� Data Link Vehicle� Launch Vehicle� Refurbishing Vehicle� Technical Summary

Page 3: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

Airborne Systems, KZO Tactical UAV System

KZO TUAV / FTS / 08.02.2006 / Chart 3Observe copyright as per ISO 16016

System Elements

Page 4: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

Airborne Systems, KZO Tactical UAV System

KZO TUAV / FTS / 08.02.2006 / Chart 4Observe copyright as per ISO 16016

Air Vehicle (1)

HW Design (1)� Compact Tail-Less Low-Set Wing

Configuration� Foldable Wings for Transport and

Refurbishing� Radar Absorbing / Radar Transparent

GFRP / CFRP Design � Thermal De-Icing through Engine Cooling Air� Booster Launch with Booster Drop after Burn-Out� Parachute / Air Bag Landing

Page 5: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

Airborne Systems, KZO Tactical UAV System

KZO TUAV / FTS / 08.02.2006 / Chart 5Observe copyright as per ISO 16016

Air Vehicle (2)

HW Design (2)� Front Section of IR-Payload (Camera and Stabilisation Platform)

connected to Air Frame by means of a Manacle Ring� All Electronics in one Unit for easy Access for Maintenance� On-Board Electronic Unit (Flight Control System, Payload Electronics,

Video Tracker, Video Data Compression, Video Data Recorder , GPSReceiver) in one Housing

� ADT-ELU, Crash-Recorder and IMU mounted to Housing of On-Board Electronic Unit

� Flight Control by Dead Reckoning updated by Rho-Theta Measurement of DLV, Need for GPS only for Reconnaissance “Behind the Hill”

Page 6: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

Airborne Systems, KZO Tactical UAV System

KZO TUAV / FTS / 08.02.2006 / Chart 6Observe copyright as per ISO 16016

Air Vehicle

Characteristics� Wing Span 3.4m� Width (transport) 1.0m� Length (flight) 2.3m� Height 1.0m� Take-Off Weight 161kg� Payload Weight 35 Kg

Page 7: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

Airborne Systems, KZO Tactical UAV System

KZO TUAV / FTS / 08.02.2006 / Chart 7Observe copyright as per ISO 16016

Air Vehicle

Payload Characteristics (2)� Camera

� Infra Red 8 -12 µm� 96 x 4 Detector Elements� 576 x 768 Pixel (Interlaced) � Zoom 1:8 with the following

pre-selected FOV (v x h)– Wide FOV 28,8°x 38,4°– Mid FOV 10,1°x 13,5°– Narrow FOV 3,6°x 4,8°

� Video Tracker (Correlation or Cycloid)� Digital Video Data Recorder, 10 min Recording Time

(Compressed Video Data incl. PID)

Page 8: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

Airborne Systems, KZO Tactical UAV System

KZO TUAV / FTS / 08.02.2006 / Chart 8Observe copyright as per ISO 16016

Ground Control Station

Page 9: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

Airborne Systems, KZO Tactical UAV System

KZO TUAV / FTS / 08.02.2006 / Chart 9Observe copyright as per ISO 16016

Ground Control Station

Characteristics� Three Identical Operator Stations for Online / Real Time Mission

Planning and Mission Modification, Flight Control and Image Exploitation

� Sheltered for EMI, NBC and NEMP Protection� Air-Conditioned 15ft ISO-Standard � Height Adapted to Road-/Railway-Transportation

� External Power Supply by Towed GPU, Supply during Transport Possible to Handle extreme Temperatures, Internal Uninterruptible Power Supply (UPS)

� Transportable by � Truck (5t Payload)� Railway� A/C (C130, C160)

Page 10: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

Airborne Systems, KZO Tactical UAV System

KZO TUAV / FTS / 08.02.2006 / Chart 10Observe copyright as per ISO 16016

Ground Control Station

HW Design and Architecture

Page 11: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

Airborne Systems, KZO Tactical UAV System

KZO TUAV / FTS / 08.02.2006 / Chart 11Observe copyright as per ISO 16016

Ground Control Station

FunctionMission Planning

Listing of Mission Elements:Shows the arrangement ofthe mission

Map functions

Toolbox with buttons formission planning

Draw function

Page 12: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

Airborne Systems, KZO Tactical UAV System

KZO TUAV / FTS / 08.02.2006 / Chart 12Observe copyright as per ISO 16016

Ground Control Station

FunctionFlight Control &Mission Modification

Listing of Mission Elements:Shows the arrangement ofthe mission

Map functions

Toolbox with buttons formission planning

Draw function

Page 13: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

Airborne Systems, KZO Tactical UAV System

KZO TUAV / FTS / 08.02.2006 / Chart 13Observe copyright as per ISO 16016

Ground Control Station

FunctionExploitation ofRecorded Video

Image Enhancement

Video Replay Control

Payload Control

Page 14: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

Airborne Systems, KZO Tactical UAV System

KZO TUAV / FTS / 08.02.2006 / Chart 14Observe copyright as per ISO 16016

Data Link Vehicle

HW Design

Page 15: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

Airborne Systems, KZO Tactical UAV System

KZO TUAV / FTS / 08.02.2006 / Chart 15Observe copyright as per ISO 16016

Data Link Vehicle

Characteristics� Deployment Time 20 min� Evacuation Time 20 min� Mast System with Automatic Alignment Capability by Means of

Inclinometer (11 m High)� Ground Data Terminal� Data Link Vehicle Control Unit with Build-In Test and Indication of

GDT HW Status / Faulty LRU’s� I/F to Ground Control Station for Transmission of TM, TC and Video

Data to Air Vehicle� Connected to GCS by means of Rugged Fibre Optic Cable � Autonomous Operation with Internal Power Supply� EMV/NEMP, NBC Protection

Page 16: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

Airborne Systems, KZO Tactical UAV System

KZO TUAV / FTS / 08.02.2006 / Chart 16Observe copyright as per ISO 16016

Data Link Vehicle

Ground Data Terminal� Ground Data Terminal for

� TM, TC and Video Data Transmission to the Air Vehicle

� Air Vehicle Position Measurement� Weight: 164 kg� Testability in Accordance to VG 95 287

Page 17: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

Airborne Systems, KZO Tactical UAV System

KZO TUAV / FTS / 08.02.2006 / Chart 17Observe copyright as per ISO 16016

Data Link

Telecommand, Telemetry & Video

Page 18: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

Airborne Systems, KZO Tactical UAV System

KZO TUAV / FTS / 08.02.2006 / Chart 18Observe copyright as per ISO 16016

Launch Vehicle

HW Design

Page 19: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

Airborne Systems, KZO Tactical UAV System

KZO TUAV / FTS / 08.02.2006 / Chart 19Observe copyright as per ISO 16016

Launch Vehicle

Characteristics � Transport of Air Vehicle to Launch Site (Shock and Vibration Isolated) � Time for Launch on Launch Site < 10min� Launch Control System

� Automatic Pre-Flight Test of the Air Vehicle before Launch� Automatic Launch Sequence� Operated by Touch Screen

� Testability in Accordance to VG 95 287

Page 20: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

Airborne Systems, KZO Tactical UAV System

KZO TUAV / FTS / 08.02.2006 / Chart 20Observe copyright as per ISO 16016

Refurbishing Vehicle

HW Design

Page 21: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

Airborne Systems, KZO Tactical UAV System

KZO TUAV / FTS / 08.02.2006 / Chart 21Observe copyright as per ISO 16016

Refurbishing Vehicle

HW Design� 15ft ISO-Shelter

� Air-Conditioned � Height adapted for Road-/Railway-Transportation� EMI, NBC and NEMP Protection

� Truck (5t Payload), Off-Road� Automatic Test System for Air Vehicle Test� External Power Supply by Towed GPU, Supply during Transport

Possible to Handle extreme Temperatures, Batteries for Air Vehicle Engine Start, and Supply of Test System in Case of GPU Failure

Page 22: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

Airborne Systems, KZO Tactical UAV System

KZO TUAV / FTS / 08.02.2006 / Chart 22Observe copyright as per ISO 16016

Air Worthiness Certification

Requirements for Air Worthiness Certification for Peace Time Operation in Germany� Probability to Leave the Assigned Area shall be ��1 x 10-5/h� Probability for an Uncontrolled Flight or Crash shall be ��1 x 10-5/h� Failure Rate of Flight Path Monitoring shall be ��1 x 10-3/h� In Case of a Technical Failure which may Endanger Flight Safety an

Emergency Procedure / Emergency Device shall be Foreseen � Probability for the Activation of the Emergency Procedure /

Emergency Device shall be ��2 x 10-3/h� The Failure Rate of the Emergency Procedure /

Emergency Device shall be ��1 x 10-5/hConditions for Air Worthiness Certification � Launch and Landing in Restricted Ground Areas� Flight in Restricted Air Space

Page 23: KZO Tactical UAV System Overview 2006-01 · Characteristics Deployment Time 20 min Evacuation Time 20 min Mast System with Automatic Alignment Capability by Means of Inclinometer

Airborne Systems, KZO Tactical UAV System

KZO TUAV / FTS / 08.02.2006 / Chart 23Observe copyright as per ISO 16016

Technical Summary

� Day and Night / Nearly all Weather Operation, De-Icing� Stealthy Air Vehicle, Radar & IR - Reduction� High Precision Navigation and Target Localisation, with and w/o GPS� High Jam-Resistant Digital Data Link� No Airfield and no Additional Landing Aids Required, Precise Landing� Safe and Reliable Start and Landing, Booster / Parachute� Highly Automated Mission Planning� Computer Aided Sensor Control� Target Tracking / Image Enhancement� Rapid Deployment of System� Hand-Over Operation / Dual UAV Control � 24 h Observation� Interface to C3I-system