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EAGLE EYE
Multi-Functional, Transformable, Unmanned Aircraft
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We have developed a revolutionary new layout for drones, in which the one-piece fuselage and instrument compartment can be used on any of our drones. The antenna unit and sensors remain unchanged, which makes up 80% of the cost of any drone.
The aerodynamic scheme is the most important aspect of any aircraft, which is why we offer the flexibility to alter the drone to fit your needs. Before flight, you can completely alter the configuration of the aerodynamic surface by adding wings or blades -- changing it from an airplane to either a helicopter or a quadcopter, thus increasing its speed or power. There is more than 20 basic layout options, each of which corresponds to a specific task and load.
ABOUT
TYPE LAYOUTS
X-Wing
Tailless Airplane
Quadcopter
Motor Glider
Plane #1
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Eagle Eye Quadcopter
SKU:EE001
$
$
Price on request

Quadcopter
(analogues – the DJI Company aircrafts) is designed for vertical take-off, landing, hovering and flying at low speeds. Due to having the propellers with a significant proportion of reactive component, it is able to fly at altitudes of more than 10 thousand meters. It is characterized by high power-to-weight and thrust-to-weight ratios (up to 2-3), good controllability over all three spatial axes, sensitivity to ascending currents (as a rule, not more than 5 m/sec in normal position).

It is intended for inspection of separate objects located at heights up to 19 685 ft.

The placement of additional payload (high-resolution cameras, additional batteries, small loads and / or parachutes) is provided for on the external mount.
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Eagle Eye Airplane with an X-wing
SKU:EE002
$
$
Price on request

Airplane with an X-wing
(analogues – the MAI airplane with an X-wing and the Shkval-1A project airplane of the Sukhov Design Bureau, barring the HERO-400EC ammunition) is intended for vertical take-off, landing and hovering in two modes – vertical ("helicopter") and horizontal ("airplane"). It is characterized by low inductive resistance, high power-to-weight and thrust-to-weight ratios (up to 2-3), good controllability over all three spatial axes. Due to the large critical angle of attack, it is not very sensitive to ascending and descending flows, which allows it to fly in conditions of large-scale turbulence, for example, directly near mountain slopes or in cumulus clouds. The presence of four wing consoles allows it to fly at altitudes of more than 32 808 ft.

It is designed for flights in conditions of strong turbulence, with strong ascending and descending currents in mountains at altitudes of more than 14 763 ft. It is able to fully operate where piloted aircrafts and traditional unmanned aerial vehicles are helpless.

This configuration (layout) is distinguished by: high values of critical angles of attack, symmetry of aerodynamic characteristics along all axes, good controllability, ability to carry out vertical take-off and landing.

The main purpose is air support of search and rescue operations in the mountainous terrain at high altitudes.

Special feature of the instrument compartment is the Flir Boson thermal imager.

The placement of additional payload (containers for medicines capable of removing oxygen starvation or for small loads) and/or parachute is provided for on the external mount.
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Tailless airplane
SKU:EE003
$
$
Price on request

Tailless airplane
is one of the main types of small unmanned aircrafts intended for aerial photography and monitoring the earth's surface (analogues – Horten Ho IX (1940), Northrop N-1M (1940), B-49 (1946), Northrop B-2 Spirit (1989), unmanned aircrafts of Geoscans and ZALA companies). It differs in simplicity of design, small specific wing load, and difficulty of manual control.

The main purpose – monitoring the earth surface, aerial photography, creation of three-dimensional image, cartography, search operations at a distance (height) of at least 656 ft from the surface of the earth (slopes), etc.

Features of the instrument compartment – higher resolution camera with the between-lens shutter, thermal imager

External mount can be used for extra payload – additional accumulators, radiation environment and harmful atmospheric admixtures monitoring sensor, and / or a parachute

It is designed for flights in a relatively calm atmosphere at altitudes of up to four thousand meters.

Features of design and configuration (in comparison with the X-wing airplane):
  • reduced value of the wing specific load;
  • increased weight of the permitted payload;
  • reduced number of drive motors – reduced energy consumption and increased flight time and range;
  • simplicity of construction.
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Plane #1
SKU:EE004
$
$
Price on request
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Motor glider
SKU:EE005
$
$
Price on request

One-piece fuselage motor-glider
is an excellent option for long flights, including high altitude ones, in a relatively calm atmosphere. Analogues – MQ-9 Reaper, Predator, X-UAV Talon, Orion-E drones. It works well for retransmission of radio signals, long-term monitoring of the earth's surface. This scheme is successfully used in aircrafts with electric motor and solar panels.

The main purposes are signal retransmission and ground surface monitoring

Features of the instrumentation compartment – signal repeater and / or higher resolution camera with the between-lens shutter.

External mount can be used for extra payload – additional accumulators, radiation environment and harmful atmospheric admixtures monitoring sensor and / or a parachute.

It is designed for flights in a calm atmosphere at high altitudes and away from the slopes of the mountains.

Features of design and configuration (in comparison with other modifications of the device):
  • the lowest load on the wing;
  • the lowest power consumption level;
  • the longest flight time ensures hovering of the aircraft above the desired point or area and retransmission of the signal downward (for example, to the aircrafts occupying lower flight levels) for a long period of time.
Our fleet of un-manned aircrafts are able to cope with almost any task within the field of aerial operations, thanks to the availability of flexible tuning of the aircraft's aerodynamic schema.
IMPLEMENTATION
Aerial Photography of the Terrain and the Creation of Its Three-Dimensional Images
1
Aerial Support For Search and Rescue Operations in Difficult Meteorological Conditions (Especially In the Mountains and At Sea)
2
Application of Aerological Research
3
Inspection of Clouds
4
Examination of the Combined Acquisition of Data from Both Airborne and Ground-Based Vehicles
5
Investigation Focusing on the Aerodynamic Shapes of Unmanned Vehicles (Intended for Operation Under Different Conditions)
6
Aerial operations are not the only performance of which our UAVs are capable. Further, we offer a variety of options that carry out integrated studies -- in which aerial, land, and water resources are involved. For example, our UAVS are able to monitor both bodies of water and shorelines. Moreover, our vehicles can be used to determine both the state of the shoreline, as well as the recommended monitoring boundaries (i.e., where there is no "clutter" of the reservoir). In short: our ground and water surface vehicles (i.e., unmanned floating crafts) are seamlessly able to monitor the condition of the reservoir itself.
Route of Any Floating Crafts (Based on Aerial Reconnaissance Data)
Depth Map
Oxygen Content
The comparative technical characteristics of our designs are provided in the table below:
CHARACTERISTICS
Characteristics
Quadcopter
X-wing
Tailless
Motor glider
Flight Height (At Least FT)
19685
32808.4
19685
19685
Flight Speed (At Least FT/S)
65
115
65
33
Accumulators (Not Less Than Type/MAH)
Li-Io/11000
Li-Io/11000
Li-Io/11000
Li-Io/11000
Number of Motors
(Brushless Electrical)
4
4
1
1
Specific Wing Load (a Maximum of G/DM2, Depending on the Payload)

-
~120
~71
~34
Payload
In Accordance with Flight Assignment, Please Refer to the Nomenclature Below.
In Accordance with Flight Assignment, Please Refer to the Nomenclature Below.
In Accordance with Flight Assignment, Please Refer to the Nomenclature Below.
In Accordance with Flight Assignment, Please Refer to the Nomenclature Below.
Flight Time (at Basic Minimum)
25
25
60
90
Wind Speed at Take-off (a Maximum of FT/SEC)
50
100
65
65
Type of Takeoff / Landing
vert. / vert., net
vert. / vert., net
Catapult or From Hand / Parachute
Catapult or From Hand / Parachute
Geometrical Dimensions, (LxWxH), Inches
19.685х19.685х7.87
19.685х19.685х19.4882
48х27х5.5
79х43х9.8
WEIGHT, POUNDS, Approximate
~4 (Depending on Configuration and Payload)
~4 (Depending on Configuration and Payload)
~4 (Depending on Configuration and Payload)
~4 (Depending on Configuration and Payload)
A huge variety of tasks and functions for our aircrafts dictate the need for a wide variety of assembling options for the central component of the machine: its instrument compartment. Just like the exterior of our aircrafts, the inner configuration can be directly modified during flight preparations.

As a matter of convenience, we have combined all options for equipping the instrument compartment within two groups: constant filling (i.e., it does not change when the aerodynamic configuration of the aircraft and / or the flight assignments are changed) and variable payload (i.e., it remains contingent upon the user's preference; in addition, it is dependent upon the specific flight objectives).
INSTRUMENT COMPARTMENT
Constant payload
  1. Flight controller – the Holybro PixFalcon Flight Controller (OSD, GPS, Telemetry) Combo or NAVIO2 (PXFmini) types, together with a single-board computer such as Raspberry.
  2. FPV panoramic camera – the Podofo HD 360 type, with AV output.
  3. Video transmitter – the Lawmate 2 GHz 8-CHANNEL 1000 MW (12 km) type.
  4. Radio receiver – the TBS CROSSFIRE DIVERSITY BUNDLE (SPECIAL OFFER) type, 15 km.
  5. GPS beacon – the tBeacon Amber.
  6. LC filter – the LC filter 2A 16V type.
  7. Voltage stabilizer (regulator) (3.2 V) – the LM2596 type.
Variable payload
  1. Precision positioning system (RTK – Real Time Kinematic) – the SinoGNSS (manufacturer ComNav Technology Ltd) type.
  2. Radio modem – RFD-900 (up to 40 km) type.
  3. Multiscreen display system, 4 video channels – the 2D, 3D multi-view video system type.
  4. Video channel switch – the 3-channel FPV Video Switcher type.
  5. FPV video camera – the RunCam Eagle 2 Pro type.
  6. Side photo and video camera – the RunCam Split V2 type
  7. Stern video camera – the RunCam Micro Sparrow FPV Camera 16: 9 CMOS 700TVL with OSD type.
  8. Night camera – the RunCam Night Eagle type.
  9. Night video camera – the Runcam Owl 700TVL type.
  10. Thermal Imager – the Flir Boson or Flir Quark 640 type.
  11. Video recorder – the HM Digital Video Recorder type.
  12. I2C interface expander – the FrSky FSH-01 type.
  13. Laser altimeter – the SF11 / C (120 m) type.
  14. Flight mode switch – the Switcher for APM, Px4 and Pix autopilots type.
  15. Type K thermocouple signal converter (chromel-copel, -200…+1300 ⁰C) – the MAX6675 type.
  16. Sensors:
  • ground speed (wind) measurements – the Pixhawk Digital Airspeed Sensor w/ Pitot Tube type;
  • outside temperature measurement – the WZP PT100 – A (-200…+300 ⁰C) type;
  • external pressure measurement – the PS002 type;
  • radioactivity measurement – the Flycamuav type;
  • various gases concentration (chlorine, methane, diesel fuel, carbon monoxide, oxygen, hydrogen sulfide, carbon dioxide, nitrogen dioxide, sulfur dioxide, ozone, VOC) measurement – Flycamuav type.
Installation and connection of other equipment are possible by individual request of the user – we are ready to provide a full catalog upon your request.