QRS FOR MICRO UNMANNED AERIAL VEHICLE (UAV) SYSTEM (60 Minutes)

Parameter Specifications 1 Micro UAV system should consist of the following sub-systems:- 1.1 UAV Bird with battery pack 1.2 Ground Control station with data link equipment 1.3 Daylight Camera Payload 1.4 1.5 2 2.1 Night Camera Payload Micro UAV characteristics:- Role Universal Battery Charger with Power Supply System Surveillance, reconnaissance and detection during day and night. 2.2 Launch and Recovery mode i) Vertical Take Off and Landing (VTOL) from within an area of 25m x 25m clearing or less. ii) Payload should not damage during recovery of UAV 2.3 Aural Signature ≤40dbs at 300 meters Above Ground Level 2.4 Payloads capability carrying Should have capability to carry electro Optic (EO) for day and Thermal Imager (TI) for night one at a time. or 2.5 Flight Modes Integrated day & Night payload. (As per user requirement) a) Fully Autonomous Vertical Take Off b) Fully Autonomous Vertical Landing c) Hover at defined waypoint d) Autonomous waypoint navigation (pre-defined as well as dynamically adjustable waypoints during flight) 2.6 Endurance h) Fully autonomous and stabilized. g) Should be controllable in real time from the GCS up to recovery. f) Vision based Autonomous Target Tracking of fixed and moving targets. e) Remote Piloted mode for video based user navigation. 60 minutes or more with all payloads at Mean Sea Level. hata workn DeS f 785897//2024FFRDCERANCH -2- SN Parameter 2.7 Operating Altitude Specifications 400m AGL (Above Ground Level) or more. 2.8 Launch Altitude 2000m AMSL (Above Mean Sea Level) or more 2.9 2.10 Range of Operation Cruise Speed Minimum 5 km line of sight 25 km/h or more 2.11 Operating Conditions Wind a) Take off: 20 km/h or more b) Landing: 20 km/h or more c) Operate: 20 km/h or more 2.12 Failsafe features a) Automatic Return to Home on communication failure b) Automatic Return to Home/Land on low battery c) Multiple GPS on-board for GPS failure redundancy 2.13 Propulsion system Electrical with rechargeable batteries 3. Payload characteristics:- 3.1 Payloads required a) Electro Optic (EO) for day (colour) b) Thermal Imager (TI) for night or c) Integrated day & night payload. (As per user requirement) 3.2 Payload and Video Stabilization a) All payloads should be gimbals stabilized onboard. b) Video output should be digitally stabilized at all zoom levels. c) Quality of video should not be affected by UAV vibrations. 3.3 Electro optic (EO) Daylight Payload a) Colour Camera with 360° pan and 90° tilt control during flight. b) Resolution: 1280 X 720 pixel or better Gr aks waRm 785297024FRDCERANCH SN Parameter -3- Specifications c) Optical Zoom: 10X zoom with minimumFOV≤5°, maximum-FOV ≥ 45° (wide field). Digital zoom: 4X d) Should be able to detect human size target at 750 meter slant or more 3.4 Thermal Imager (TI) Night Payload a. Thermal Camera with 360° pan and 90° tilt control during flight. b. Resolution: 640 X 480 pixels or better c)White/Black Hot modes d) Digital Zoom: 4X or more e) Should be able to detect human size target at 400 meter slant or more 3.5 Night Beacon Recovery Switchable (from GCS) LED light when operating with Night Payload 4. Ground Control Station characteristics:- 4.1 Option-1: GCS should have MIL-STD-810G or better and IP51 better, semi rugged laptop. or Option-2: GCS should have MIL-STD-810G or better and IP65 or better, rugged laptop. (As per user requirement) 4.2 Computing Hardware :- CPU Intel Core i5 v Pro Processor, 2.3 GHz or better Storage Minimum 500 GB Memory Display 4.3 4.4 4.5 4.6 Keyboard & input Battery Operation Battery Charging time of GCS Data portability Interface 在 2GB or more Minimum 10 inch - 1024 x 768 XGA sunlight readable screen, anti-glare. Touch screen Minimum 02 hours at peak utilisation. Should be less than 3.5 hours Ports for data transfer to external secondary storage devices VGA/HDMI, USB, 10/100/1000 Ethernet. wolRm 785897//2024FFRDCERANCH SN Parameter 4.7 Capability -4- Specifications a) Transmit control commands to UAV. b) Receive UAV flight and propulsion parameters. c) Receive, display and record real time day and night video from UAV. d) Capability to control UAV while on the move. 4.8 GCS Application Software a) Geographic Map along with UAV location, UAV trajectory, camera view polygon, waypoints and flight plan. 4.9 Map Formats b) Real-time video from the UAV with onscreen display of important parameters like:- i. Coordinate of target ii. Ground altitude of target iii. UAV Position iv. Height of UAV above ground level v. Distance of UAV from GCS vi. Bearing (Azimuth) of UAV from GCS vii. Ground speed of UAV viii. UAV Heading/ True North indication ix. Mission time c) Geographic map and real-time video should be displayed at all times during the flight. d) Geographic map and real-time video views should be resizable and/or switchable to allow user to switch between big map/small video and small map/big video views through a single click/button input. e) Artificial Horizon indicating UAV altitude. f Switchable between 2D/3D views, capability to Tilt/rotate 3D map as per user input. a) Should have the capability to integrate geo-referenced raster maps provided in at least one of the commonly used digital map formats (GIF, TIFF, DTED and SRTM etc.) b) Should be able to work with Google Maps, application should have the capability to download maps automatically after specifying location GPS co-ordinates. haks wRm Qiter Ser ey 1 785397/2024FRDCERANCH -5- SN Parameter Specifications 4.10 Payload Controls a) Selection and switch on/off of payload b) Pan/Tilt/Zoom Controls c) Point payload to ground co-ordinate function d) Recording on/off e) Switch on/off Night Recovery Beacon 4.11 Joystick Controls i. Full Camera Control 4.12 Video Pan/Tilt Zoom In/Out Black/White Hot ii. RPV Mode iii. Altitude Control a) Video should be recorded in any commonly portable video formats (AVI/MPEG/ MP4 etc) b) Video of the full flight should be recorded c) Should have capability to take image snapshots at any time during flight d) Software should be provided that will facilitate extraction of imagery from the recorded video post flight 4.13 Pre-flight checks Self-test of UAV system, Output: go/no go 5. Communication Link:- 5.1 Communication link equipment capability i) Transmit control commands from GCS to UAV ii) Transmit parameter of UAV and payload to GCS iii) Transmit day and night video from UAV to GCS 5.2 Type of link Secured digital uplink & downlink with AES encryption. 5.3 Frequency Band System should operate on S & C frequency Band uplink and down link, preferably on license free band i.e 2.4Ghz or 5.8 Ghz. 6. General System requirements:- 6.1 Weight The weight of complete Micro UAV bird including battery pack & one payload should ≤ 6kg. 6.2 Assembly/ Disassembly time Less than10 minutes each. 6.3 Life of Micro UAV The total technical life of micro UAV should not be less than 500 landings. 3 one Shake er 785397//20244FF&DCERANCH SN Parameter 6.4 Environmental Conditions for Operation and Storage 6.5 Portability and Operation 6.6 6.7 6.8 Battery of AV Battery Charger of AV battery Accessories Maka WO/RM R.S.Dhaka Assam Rifles -6- Specifications The UAV and associated systems should be certified for operation and storage for following environment conditions. i) Damp Heat: 40 °C at RH not less than 95% ii) Operating temperature & Storage temp: -10°C to +55°C iii) Ability to withstand dust, drizzle and humid conditions The Micro UAV should be battery operated portable, light in weight, compact, for day and night surveillance, capable of being carried and operated by two men. The intelligent standard lithium based battery pack should have the backup of minimum 60 minutes. Suitable universal battery charger to charge the batteries within two to three hours. a) Water proof Back Packs IP66: 1 set b) Field Repair kit: 1 No's c) Lithium based Battery packs: 3No's d) Spare propeller Sets: 2 No's e) Spare Landing Gear sets: 2 No's f Associated Cables & Mountings: 1set g) Hard transportation boxes: 1set h) User, Technical & Maintenance Manual:11set i) Log book: 1 set goe INSP/T V.K.Kothiyal BSF Aefea INSP.Rajeev Dahiya CISF eel J.K.Sharma, DC(MOЕ) SSB P.R.Jha,DC(UAV) CRPF B.N.Sonawan, Se 2 I/C ITBP Raju Bhargava. IPS, IG(Comn &IT), CRPF fay Harjinder Singh,DIG(Eqpt) CRPF D.S.Rawat,DIG(Comn) CRPF 0 R.P.Singh. ghe IPS, SDG(Comn) CRPF Approved/Not Approved hm Rajeev Rai Bhatnagar, IPS DG, ORPF .ו!