ESTGIS 2012 Priit Leomar 1

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1 ESTGIS 2012 Priit Leomar 1

2 ELI 1995 Haljas tee 25 Tallinn Estonia ESTGIS 2012 Priit Leomar 2

3 MAIN ACTIVITIES ELI ELI MILITARY SIMULATIONS ELI ENGINEERING ELI AIRBORN SOLUTIONS ESTGIS 2012 Priit Leomar 3

4 SWAN III ESTGIS 2012 Priit Leomar 4

5 UAV SWAN III UAV research and development program (SWAN I) in Estonia was initiated by the Estonian Defence Forces and delivered by ELI Ltd. The next generation SWAN II offers further enhanced capabilities for surveillance and reconnaisance ESTGIS 2012 Priit Leomar 5

6 FUNCTIONALITIES of SWAN III border patrol aerial photography geophysical prospecting disaster monitoring coast guard services day/night reconnaissance battlefield monitoring target positioning artillery spotting battlefield damage and casualty assessment ESTGIS 2012 Priit Leomar 6

7 SYSTEM CAPABILITIES Real time video from gyro stabilized gimbal On board video recorder Stabilized digital photo camera Fully autonomous flight control including takeoff and landing Autonomous mission execution with option to change all parameters during flight Ability to select active waypoints and/or change waypoint coordinates and parameters Different preprogrammable flight patterns Definable actions in case of errors and loss of data link (Return Home, Proceed with Mission, Emergency landing after critical error etc.) Multi sensor usage Fast and easy takeoff by catapult Low noise and weak radar footprint Controllable navigation lights ESTGIS 2012 Priit Leomar 7

8 MAIN COMPONENTS OF UAV SYSTEM SWAN III 1. Ground segment GCS (Ground Control Station) Catapult for launching the UAV Antenna tracker for video link 2. Air segment Air vehicle ESTGIS 2012 Priit Leomar 8

9 AIR VEHICLE SWAN III Weight: kg Length: 190 cm Wing Span: ca 300 cm Power: four stroke Aero Engine Cruise Speed: 100 km/h Endurance: ca 6 h Radius: ca 100 km ESTGIS 2012 Priit Leomar 9

10 AIR VEHICLE SWAN III Wingspan 3.075m Length 1.960m Weight 12 15kg Engine 4.0hp 35cc 4 stroke Gyro stabilized gimbal Video Video camera IR camera Dual gimbal option Photo Gyro stabilized mechanism Min Max Operational ceiling 150m 2500m Range - 150km* Flight time - 180min* Fuel capacity - 3.0L Speed 80 km/h 130 km/h* Wind - 7 m/s Datalink range - 50km* Videolink range - 40km* ESTGIS 2012 Priit Leomar 10

11 GIMBAL Video IR Photo Type FCB-EX20D SONY TAU 640 FLIR DMC-GF1C Panasonic Resolution PAL 530 TV lines 640x512 12MPix Zoom 10x opt. 8x digital - Sensitiv ity 0.25lx 1/60s <50 mk at f/1.0 with FLIR proprietary noise reduction F2.0 ISO /1.6 Controlling Gyro + GPS Gyro + GPS Gyro Data storage >4h >4h >2000 images* Nose-mounted gimbal with color camera or IR camera is used for remote piloting, and for automatic navigation allowing 180 degree operability of the camera in both horizontal and vertical direction ESTGIS 2012 Priit Leomar 12

12 DIGITAL CAMERA Video IR Photo Type FCB-EX20D SONY TAU 640 FLIR DMC-GF1C Panasonic Resolution PAL 530 TV lines 640x512 12MPix Zoom 10x opt. 8x digital - Sensitiv ity 0.25lx 1/60s <50 mk at f/1.0 with FLIR proprietary noise reduction F2.0 ISO /1.6 Controlling Gyro + GPS Gyro + GPS Gyro Data storage >4h >4h >2000 images* ESTGIS 2012 Priit Leomar 13

13 DIGITAL CAMERA ESTGIS 2012 Priit Leomar 14

14 ESTGIS 2012 Priit Leomar 15

15 ESTGIS 2012 Priit Leomar 16

16 ESTGIS 2012 Priit Leomar 17

17 ESTGIS 2012 Priit Leomar 18

18 ESTGIS 2012 Priit Leomar 19

19 ESTGIS 2012 Priit Leomar 20

20 ESTGIS 2012 Priit Leomar 21

21 PARACHUTE ESTGIS 2012 Priit Leomar 22

22 PARACHUTE RELEASE SYSTEM ESTGIS 2012 Priit Leomar 23

23 ESTGIS 2012 Priit Leomar 24

24 ESTGIS 2012 Priit Leomar 25

25 AIR BAG ESTGIS 2012 Priit Leomar 26

26 ESTGIS 2012 Priit Leomar 27

27 TRANSPORT AND STORAGE ESTGIS 2012 Priit Leomar 31

28 MANPAD (MAN PORTABLE GROUND CONTROL SYSTEM) ESTGIS 2012 Priit Leomar 34

29 BATTERY CHARGING UNIT ESTGIS 2012 Priit Leomar 35

30 MAN PORTABLE GROUND CONTROL SYSTEM ESTGIS 2012 Priit Leomar 37

31 ESTGIS 2012 Priit Leomar 38

32 ESTGIS 2012 Priit Leomar 39

33 ESTGIS 2012 Priit Leomar 40

34 VIRTUAL COCKPIT ESTGIS 2012 Priit Leomar 41

35 ANTENNA TRACKER FOR SENDING AND RECEIVING DATA AND VIDEO SIGNALS ESTGIS 2012 Priit Leomar 43

36 ANTENNA TRACKER VIDEO ESTGIS 2012 Priit Leomar 45

37 CATAPULT LAUNCHER ESTGIS 2012 Priit Leomar 46

38 CATAPULT LAUNCHER VIDEO ESTGIS 2012 Priit Leomar 48

39 UAV SWAN III ESTGIS 2012 Priit Leomar 49

40 CATAPULT VIDEO ESTGIS 2012 Priit Leomar 50

41 DIRECTION FINDING SYSTEM FOR TRACKING ESTGIS 2012 Priit Leomar 51

42 ELIX4 MULTIRORTOR ESTGIS 2012 Priit Leomar 55

43 ELIX4 MULTIRORTOR ESTGIS 2012 Priit Leomar 56

44 ELIX4 MULTIRORTOR EliKopter X4 Specifications Dimensions packed 370x210x80 Dimensions 470x470x80 Take off weight 2.5 kg Autopilot Motors MK3638 or similar Motor controllers BL-Ctrl V2.0 Min Max Comments Operational ceiling m AMSL Range - 10 km Dependant on data and video link configuration Flight time h Dependant on flight profiles and payload Battery capacity - 10 Ah Standard LiPo battery Speed - - Adjustable in flight Wind - - Measured on ground Datalink power 1 W - - Videolink Power 0.5 W 2 W Adjustable output ESTGIS 2012 Priit Leomar 57

45 ELIX4 MULTIRORTOR Video IR Photo Type FCB-EX20D FLIR Quark or TAU On demand Resolution PAL 530 TV lines 640x512 - Zoom 10x optical 4x digital - Sensitivity /60 s <50 mk, spectral band μm - Stabilization 1 axis Tilt 1 axis Tilt - Optional onboard storage >4 h >4 h ESTGIS 2012 Priit Leomar 58

46 ELIX4 MULTIRORTOR ESTGIS 2012 Priit Leomar 59

47 THANK YOU FOR LISTENING ESTGIS 2012 Priit Leomar 60

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