Pteryx_UAV Knowpia

Pteryx UAV
Pteryx UAV
	Pteryx UAV, with the camera mounted sideways.
General information
Type	UAV
Role	Photography
National origin	Poland
Manufacturer	Trigger Composites

Pteryx UAV^[1] was a Polish Miniature Unmanned Aerial Vehicle (UAV) designed for civilian use. It was manufactured and sold by Trigger Composites.^[2] The machine was both a flying remote control (RC) model and pre-programmed vehicle. It was awarded the Innowator Podkarpacia medal for innovative design in the category of micro-enterprises of the Podkarpacie region in 2010.^[3]

Origin edit

The Pteryx UAV uses a custom derivation of the FLEXIPILOT software, designed by Aerial Robotics engineering group^[4] for photomapping purposes and civilian use.

The avionics and flying platform are capable of full operational capability without using an active transmitter or ground station.

Capabilities edit

Digital Surface Model of a motorway interchange construction site.

Bezmiechowa airfield 3D Digital Surface Model

4.5km² ortophotomap extracted from data collected during 1h flight

Delivering data for generating digital elevation models using external photogrammetric software and orthorectification procedure^[5]

Delivering data for precision agriculture by creating surface maps using mosaicking software
Construction site and long-range linear mapping (up to around 40 km both ways with 2-hour flight time, reserve included)^[6]

Carrying custom research equipment

The camera mount contains either pre-installed compact digital camera or can be exchanged for other equipment.

The camera can be mounted down-looking (nadir photography) or side-looking (oblique photography).

The whole head can be tilted in flight using the RC transmitter, while reducing stabilization travel to one of the sides.

Capabilities edit

Flying multiple missions per day without being required to reprogram the autopilot, using waypoints.
Exchangeable mission package
Single button operation
Fully enclosed camera head
Ability to accommodate a weight range 200g-1000g
Takeoff by catapult
Landing through use of a parachute

Camera edit

The aircraft provides positions of the photos taken, and has storage for 8000 events. Ground-projected positions include the following error margins:

GPS position error up to 5m.
Altitude drift (up to 5m per 1 hour of flight)
Camera head stabilization precision (transients up to 5°)
Fuselage pitch due to turbulence (up to 8° during hot weather, typically 2° in winter)
Camera mounting error (typically 1–4° if not calibrated)
Heading/yaw error (the aircraft performs crabbing in presence of wind)

Typical orthophoto map precision (mean reprojection errors):

10 centimetres (3.9 in) horizontal
30 centimetres (12 in) vertical
around 2.5m global shift to be removed with a few locally measured points

Data processing strategies edit

Several data processing approaches are possible depending on application:

Direct photo examination
Non-georeferenced image stitching using free software
Using free 3D modelling services, as mentioned in examples section
Importing each photo as ground overlay in Google Earth (semi-automatic with supplied software)
Using pre-paid service based on cloud computing, yielding a result in hours (delivers Orto photomap and optionally DSM)
Local processing using specialized GIS software created specifically for large scale image mosaicking (delivers Orto photomap and optionally DSM)

Aircraft components edit

Fuselage
3-section wings with mounting screws
Horizontal stabilizer section
Parachute

Other required equipment edit

LiPo batteries
Laptop or netbook
Compact digital camera
RC controller compliant with local laws (see Radio-controlled aircraft Transmitting and Receiving Frequencies)

General characteristics edit

Masses:

Maximum takeoff weight 5.0 kg

Dimensions:^[7]^[8]

Wingspan: 2.8 m
Length: 1.4 m
Height: 0.33 m
Propulsion: brushless DC electric motor and rechargeable lithium polymer battery
Endurance: 55min with 1 kg payload, 120min with 450g payload

V speeds:

V_C: around 50 km/h
V_S: 34–38 km/h depending on TOW
V_A: 120 km/h
V_NE: 160 km/h

Flight altitude:

Service Ceiling 3000m Pteryx Lite
Service Ceiling 1200m Pteryx Pro
Cruise altitude 100–520m AGL, 250m typical – dictated by photo resolution

Handling:

Assembly time: Around 5 minutes.
Materials: Custom fiberglass composite material covered with durable red gelcoat, carbon fiber and Kevlar reinforcements, wood and other plastics. Wooden or all-composite wings are offered.

References edit

^ "Pteryx UAV". Archived from the original on 12 January 2012. Retrieved 12 May 2020.
^ "Our products - Samolot bezzałogowy Pteryx" [Our products - Pteryx unmanned aircraft]. www.t-cs.pl (in Polish). Retrieved 16 December 2023.
^ Olejnik, Marta (12 December 2010). "Innowator PodkarPacIa 2010 XII Podkarpackie Forum Innowacyjności" [Innovator of Podkarpacie 2010 XII Podkarpackie Innovation Forum] (PDF). Gazeta Politechniki [The University of Technology newspaper] (in Polish). No. 204. Rzeszów University of Technology. p. 15. Archived (PDF) from the original on 3 March 2022. Retrieved 16 December 2023.
^ "Pteryx UAV". www6.aerialrobotics.eu. Archived from the original on 10 September 2010. Retrieved 4 January 2023.
^ "Bezmiechowa 3D digital elevation model (AerialRobotics and CMP SfM Web Service)". Archived from the original on 20 July 2011. Retrieved 15 January 2011.
^ Motorway mapping mission (YouTube video)
^ "Pteryx UAV dimensions" (PDF). Archived from the original (PDF) on 3 September 2011. Retrieved 7 March 2011.
^ "Pteryx UAV - Camera Head dimensions" (PDF). Archived from the original (PDF) on 3 September 2011. Retrieved 7 March 2011.