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KZO TUAV / FTS / 08.02.2006 / Chart 1Observe copyright as per ISO 16016
KZOTactical UAV System
Overview
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
Airborne Systems, KZO Tactical UAV System
KZO TUAV / FTS / 08.02.2006 / Chart 3Observe copyright as per ISO 16016
System Elements
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
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”
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
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)
Airborne Systems, KZO Tactical UAV System
KZO TUAV / FTS / 08.02.2006 / Chart 8Observe copyright as per ISO 16016
Ground Control Station
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)
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
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
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
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
Airborne Systems, KZO Tactical UAV System
KZO TUAV / FTS / 08.02.2006 / Chart 14Observe copyright as per ISO 16016
Data Link Vehicle
HW Design
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
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
Airborne Systems, KZO Tactical UAV System
KZO TUAV / FTS / 08.02.2006 / Chart 17Observe copyright as per ISO 16016
Data Link
Telecommand, Telemetry & Video
Airborne Systems, KZO Tactical UAV System
KZO TUAV / FTS / 08.02.2006 / Chart 18Observe copyright as per ISO 16016
Launch Vehicle
HW Design
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
Airborne Systems, KZO Tactical UAV System
KZO TUAV / FTS / 08.02.2006 / Chart 20Observe copyright as per ISO 16016
Refurbishing Vehicle
HW Design
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
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
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