Model Number: | DB UAV |
---|---|
Place of Origin: | China (Mainland) |
Year Built: | 2008 |
Condition: | New |
Type: | Gyroplane |
Quick Details
Specifications
DB UAV Remote Sensing System
Ⅰ. Electric throw take-off UAV Remote Sensing System
Specifications
Name |
Parameters |
Name |
Parameters |
Dimensions |
Length*wingspan* height 1.7m*2.3m*0.3m |
Max takeoff weight |
3.5kg |
Max payload |
0.8kg |
Propulsion |
Brushless motor and electronic speed governor |
Take-off speed |
30km/h |
Landing speed |
40km/h |
Max ascent speed |
6m/s |
Cruising speed |
50-55km/h |
Max speed at sea level |
80km/h |
Max flight time |
40min |
Max Service Ceiling |
1000m |
Max Wind Speed Resistance |
8m/s (Gentle breeze) |
Automatic flying mode |
GPS Navigation |
Operating radius of imagine and data |
8km |
Operating environment |
Temperature: -10 to +45℃ Humidity: 5% to 95%(Relative) |
1. Configurations
Standard configuration: A set of UAV system(including aircraft frame, propulsion system, autopilot, onboard data communication radio, image transmission module etc. );
A set of high definition camera;
A set of ground station (Equipment box + portable computer + ground data communication radio + digital antenna + antenna tripod + ground station software + displayer of video and image + video and image receiver + antenna of automatic tracking system);
A set of operations manuals;
A set of remote controller;
A set of common tools and ground assistive device;
Packaging and transporting container;
Optional: user-specified slim digital camera
2. Features and applications
Electric throw take-off UVA has features as following:
A. Light takeoff weight, concise system which is easy to operate, user-friendly for experienced model players, easy to learn and operate;
B. Using efficient brush-less motor, electronic governor and li-po batteries, easy to operate and maintain.
C. Throw takeoff and belly touchdown landing, low in zone requirement
D. Especially useful in emergency for the quick ability of deployment and operation
Main applications:
A. Obtaining high definition videos for real time aerial monitoring
B. Can be used as an aerial photographing aircraft in particular area when carrying with compact digital camera
Ⅱ. DB2 UAV remote sensing system
Specifications:
Name |
Parameter |
Name |
Parameter |
Dimensions |
Length*Wingspan*Height 2.0m*2.m*0.6m |
Max Take-off Weight |
13kg |
Max Payload |
3kg |
Taxiing takeoff and landing distance |
20 to 40m |
Take-off speed |
55km/h |
Landing speed |
60km/h |
Stall speed |
50km/h |
Max ascent speed |
12m/s |
Max Speed |
150km/h |
Cruising speed |
100-110km/h |
Max service ceiling |
5000m |
Endurance |
2hours |
Max wind speed resistance |
Strong breeze (10.8 to13.8m/s) |
||
Automatic flying mode |
GPS navigation |
Measure radius(in intervisible) |
30km |
Propulsion system |
twin-cylinder aviation gasoline-engine |
Engine displacement |
56cc |
Fuel type |
93 or above unleaded gasoline and two-stroke lubricant |
Camera |
Canon 5DII camera + fixed lens + 2-axis stabilizatioin platform |
Gimbal accuracy |
Heading angle:≦7° Roll angle:≦3° |
||
Operating evironment |
Temperature: -20 to +50℃ Humidity: 5% to 95%(relative) |
1. Configurations
Standard configuration:
A set of UAV system(including aircraft frame, propulsion system, autopilot, onboard data communication radio, etc.);
Canon 5DII 135 professional reflex camera+2-axis stabilization platform;
(We will offer identifications and parameters for customers who need to change their lens focus);
A set of ground station(Equipment box+portable computer+ ground data communication radio+ digital antenna+ antenna tripod+ ground station software);
A set of user manuals;
A set of remote controller;
A set of common tools and ground assistive devices;
Packaging and transporting container;
Optional:
3-axis gimbal for Canon 5DII camera
Visible light camera+ 2-axis controllable gimbal
Digital images transmitting devices
Onboard micro-video recorder
Ground controller
2. Features and applications
Features:
A. Lighter weight and simple system make it easy to operate;
B.Powerful engine and short takeoff distance make the aircraft adaptive to various takeoff site ;
C. Safer for the emergency parachuting function;
D. Automatic catapult-assisted take-off and parachuting
Applications:
A. Obtaining ground true-color remote sensing images that can be used in drawing of remote sensing images;
B. Useful for missions such as lines inspection and aerial monitoring when carrying visible camera and infrared thermal imager