UAV System
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Description

 


U
nit Price
EUR

 
   D
elivery
    Approx.

 

 

 

 

 

 

 

 

 

 

 

 

1.

Standardset(inportableboxes)
OurModel
  #BXAP15
           3 pcsairframe (UAV)
                      Including on board:
                        -   Embedded PC
                        -   Autopilot
                        -   Navigation system
                        -   Two waycommunicationssystem
                        -   Telemetry&Telecommand system
                        -   Payload interface

1 pcs ground station (GCS)

Including:
              -   2 industrialPC-s (laptop)
              -   Systemcontrolsoftware
Antennatrackingsystem(BXGM11)

Otherfeatures
              -   Basiclaunchfromtheground withwheels
              -   Basiclanding(manualRCcontrolled)

5 day training
              -   Installation andoperation
             -   Upto 4 students
             -   Heldin Budapest
    Including:
            -      Trainingfacility
            -      TrainingUAV
            -      Lunch andbeverages

Not including:
       -      Traveland accommodation

Requirededucation:
          -      mediulevel (at leasBStechnicauniversity level),experience in flight modelling and composite technology usage preferred

 

















      210,000.-























   
3 -5
 months*

 

      2.

Camera with stabilised platform
      -    Day camera for day operation
      -   Day camera and uncooled thermal camera for day and night  operation


 14,990.-
  29,800.-



  
3 - 5  months*

 

     3.

Launch options
    -   With winch
    -   Catapult launch (BXGM16)

   
  5,500.-
 11,000.-

 
 3 - 5  months*

 
     4.

 Landing
     -  Automatic landing system with net

 
   18,000.-


 3 - 5  months*

 

    5.

Additional training
    -   Based on the customer request
   -   Package includes same as in the basic package

 

   12,500.- /
    5 days

 

TBD

 

 Item 1.: Basic package
 Item 2.-5.: Optional features to be selected from based on customer’s exact need. Detailed system description can be found in Appendix1.

 *Earliershipmentis possible.

 Note: The prices are for our standard model. In case of any change of the technology and/or function, the price is may also change.

 Terms & Conditions

1) Price              : Ex-works
2) Warranty      : 1 year

  • not applicable for batteries
  • valid only for intact units (not valid if there is any type of mechanical damage on the unit)
  • warranty is void in case of improper maintenance and repair

3) Payment        : T/T 30% in advance, T/T 70% at delivery
4) Validity          : 30 days


Short overview of the system

Specification and system elements

- Speed: 60-100 km/h
- Ceiling: min. 3000 m ASL (ASL: Above Sea Level) and 5000 m ASL in case of AGL < 1000 m
  (AGL: Above Ground Level)

- Wing span: 3.7 m
- Length: 1.7 m
- Take-off weight: 17 kg max.
- Endurance: up to 90 minutes
- Propulsion: electric brushless engine (1200 W peak power)
- Payload weight: up to 3 kg
- Datalink range: 20 km LOS (LOS: Line of Sight)

 

 Figure 1. - UAV (BXAP15)           Figure 2. / a - Day Camera          Figure 2. /b - Day and
                                                                                                                     uncooled thermal
                                                                                                                     camera

                                   

 

Figure 3. –Boxes for Transport and Installation:          Figure 4. – BXGM11 Antenna
                                                                                                                                       platform:

                             


Figure 5. - BXGM16 Launcher Catapult

    

Appendix1 

Basic information about your UAV system

 Airframes (Figure 1.)

The  airplane  is  made  using  the  latest  fibre  composite  technology  and  equipped  with reliable onboard electronics. Several features such as flexible route planning, adaptive communications and control mechanism are built in the system. And it has been designed to allow easy installation and operation keeping the operational cost down.

Unmanned Aerial Vehicle System (UAV) is a Reconnaissance system that can follow a pre- programmed route while sending real time video signal and position information back to the ground control station. The system is designed to be flexible and compact, therefore it is easy to transport. 

Autopilot

The system’s spirit is the autopilot. This system provides high autonomy, the BXAP15 can alone  flight  the  whole  mission.  The  autopilot  is  a  microcontroller  based  autonomous navigation unit,  which  uses GPS  for navigation and inertial sensor  for stabilization. The sensors are using modern MEMS technology, which yields small size, low weight, long operation time and high precision.

The speed is measured with a Pitot-tube. The actual geological position is allocated with a high sensitivity GPS sensor.

The altitude is measured with a high sensitivity gyroscope on board. To combination this sensors measured values can the system controlled the entire mission.

The flight  plan  can  design  on  the  ground  control  station.  The route  of autopilot  has declared with many navigation points.  After that the program made the route and the control program self and it can upload to the autopilot.

a) Flight route programming, up to 500 waypoints.
b) Real time route/flight parameter modification via radio link.
c) 3D flight control.

In Box parameters

        Size (l h)

1.95 x 0.5 x 0.8 m

Total weight (with 2 frames in the box)

50 kg

Frames per box

2 pcs


P
ayload (Figure 2. / a and /b)

We provides two standard payloads for wide application areas. These payloads have a common mechanical interface which enables fast payload replacement. These payloads have visible light or thermal cameras placed on an electromechanically stabilized gimbal system. It provides very stable video image in a wide range of situations, during different flight manoeuvres. The camera payload has basic mechanical protection against impacts.

Both cameras have four observation modes. It possibly to observe in a given angular range, automatic sweeping, to follow a chosen point, and free directional, manual controlled observe. The cached video is available real-time, and later downloaded. The real-time observation is available with the Virtual Cockpitprogram.

       

                        Day Camera                                 Day and uncooled thermal camera

 


Figure 2. / a - Day Camera

Parameter

Value

Video Output

PAL/ NTSC

Control

RS232

Zoom

x20 +x2 digital

On ScreenDisplay

Text and Graphics

StabilizationLevel

Better than 100μrad

Rangeof rotation

Pitch: -40oto +80o

Roll/Yaw: -180o  to +180o

Temperature range

-10oC to +55oC

Power Consumption

12V DC, 1.5W(typ.)

Dimensions

Diameter: 70mm

Height:80mm

Weight

150g

 


Figure2. / b-Day and Night Camera

Parameter

Value

Video Output

PAL/ NTSC

Control

RS232

Zoom

x20 +x2 digital– Daylight

x2/4 – Night (Thermal)

On ScreenDisplay

Text and Graphics

StabilizationLevel

Better than 50μrad

Rangeof rotation

Pitch: -45oto +90o

Roll/Yaw: 360ocontinuous

Temperature range

-10oC to +45oC

Power Consumption

12V DC, 4W(typ.)

Dimensions

Diameter: 83mm

Height:90mm

Weight

240g

  


GIMBAL SYSTEM

Parameter

Data

Mechanical stabilisation (PAN, TILT)

2 axes – withsemiconductor gyroscope

Electrical stabilisation (ROLL)

Optional: can beswitched on

Rotatingrange (PAN, TILT)

-180º…+180º

Rotatingspeed(in bothdirections)

300º/s(max.)

Positioningaccuracy(inboth directions)

cca. 0,05º

Resolution of  movement

cca. 0,025º

Bandwidth of mechanical stabilisation

5Hz

Vibration compensation(TILT)

24dB– with imageprocessing

Communications protocol

ViCAM

Stabilized operation mode

Fixed to vehicle / Fixeddirection / Off

Weight

appr.1,24kg

Power supply

12VDC

Powerconsumption

0,3A (typ.)

Operational temperaturerange

-10°C…+60°C

 


G
ENERAL PAYLOAD PARAMETERS

Maximum useful space(wxlxh)

180 x180x200 mm3

Maximum weight (netweight)

3 kg

Insert hole diameter

160 mm

Location ofpayload space

centreofgravity

 

Ground Station (Figure 3.)

The  UAV  ground  control  station  is  a  modular  system  which  consists  of  a  computer database server, one further computer workstations, communication equipment with antennas and mast, GPS and wind sensors and the launch catapult.

The database server and the workstation are organized in a local area network. The heart of the system is the database server, which receives processes and stores every pieces of information about the mission (telemetry data, command data, video streams, etc.).

Furthermore  the  system  contains  the  navigation  client  software,  surveillance  client software, server management software and other software utilities, which can run on the server computer or on separate workstations.

Radio communication

The UAV system has long range, reliable, robust, wireless radio communication data link. The link operates on the C band. The typical range is 20 km, but it can be extended up to 50 km. In case of LOS (Line Of Sight), the same communication technology can be used up to

100 km. The radios use highly interference tolerant one-way channel OFDM modulation for digital video signal and FM Chirp modulation for telemetry and command.

The telemetry channel is two-way channel. The telemetry data is downlink, the command line is uplink. With the Virtual Cockpit program can the pilot give some different pre-defined orders,  for  example  to  descend,  or  to  speed  up.  Robustness  is also  enhanced  the  error detection and correction coding. The communication is protected by additional scrambling for higher security.

 

fig. 7. GPS track of a 20 km distance communication test flight

 

 

 Antenna Tracking System (Figure 4.)

 

TECHNICAL PARAMETERS

RotationRange

360degreecontinuously

Max.continuousrotationvelocity

30deg/sec

Re-positionaccuracy

in 0,6deg

Operationvoltageofelectricengine

12V

Maximumoperationcurrent

1,4A

Sensationofactualposition

absolute

Data formatofactual position

12bits

Operationtemperature  range

-30…+60oC


 

Catapult launch (Figure 5.)

 

MECHANICAL  PARAMETERS

Maxphysicalsizelxwxh

7.7x1.06x1.75m

Acceleration  length

4.4m

Weightwithoutwinch

100kg

Elevationanglerange

8.5…13.3deg

Boxsizelxwxh

1.60x0.55x0.55m

Totalweight(inbox,withoutwinch)

120kg

Sizeofwinchbox*

0.6x0.4x0.4mapp.

Weightofwinch(inbox)*

25kgapp.

*The winch is supplied only if the customer requires.

TRAINING

Basic knowledge of installation and operation

→ Mission

  - Checklist
  - Unpacking at site and prepare for flight  
  - Pre-flight check  
  - Mission planning and uploading to system  
  - Mission execution
  - After flight

→ Maintenance

  - Airframe (Wing, horizontal-stabilizer Fuselage)
  - Propulsion (Engine / Propeller)

Elementary RF communication lessons

Basic theory of aviation

Classroom training and simulations

→ Software

  - Ground control software system operation
  - Ground control software system installation, backup
  - Map management
  - Autopilot configuration
  - On-board computer software installation and configuration
  - Programming and testing of on-board digital circuits
  - On the job training
  - Basic maintenance lessons

 

Operation in practice

Course takes 5 days

 

 

Thermal picture                                                Moving object tracking

        

 

Fix object Tracking / Flight path visulization on ground station

        

       

 

 

 

Kapcsolat


 H-6000 KECSKEMÉT, 
 Dobó krt. 5. 4/12., Hungary


 +36-70-408-55-00 (magyar, orosz)
 +36-30-644-77-74  (magyar, angol)


+36-76-509-070


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