TGT
// DRONE TARGETING AND DELIVERY SYSTEM
OrbEye
Ground to target.
60 seconds.
SYSTEM ACTIVE
RANGE: UP TO 1000 M  |  ACCURACY: ±3 M  |  TIME: <60 S
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// MISSION

Autonomous delivery of a strike drone
to the point of impact —
without manual piloting.

OrbEye solves one task: the operator selects an object on the launcher screen. The drone launches and destroys the target in 60 seconds.
60
seconds
from launch to strike
1
destroyed
target
1
operator
dispatcher, not pilot
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// PROBLEM

Standard approach —
is the weak link.

3–5 min
Deployment time
Manual takeoff, orientation, getting into position — the time varies every time.
±15 m
Positioning accuracy
The pilot aims by eye. In wind and dense urban areas — errors are critical.
1 pers.
Operator required
Fatigue, human factor — dependence on a single link.
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// SOLUTION: 4 PHASES

One protocol. Repeatable result.

PHASE 01 — AIM
Aim
The operator indicates the object on the launcher screen. The system locks onto the visual target and prepares the launch profile.
T-0 → T-5 s
PHASE 02 — LAUNCH
Launch
Pneumatic launch: 0 → 90 km/h in ~0.1 s (1.2 m tube). G-force ~27g. Initial ballistic trajectory.
T = 0 s  |  ~27g
PHASE 03 — CRUISE
Cruise
Onboard leveraging AI and computer vision tracks the object via video stream. Autopilot maintains course and speed at 80–90 km/h.
T+1–55 s  |  Ieveraging AI and computer vision TRACK
PHASE 04 — DESTROYED
Destruction
AI Computer vision. Arrival at the contact point. Detonation. Target destroyed. Status OBJECT_DESTROYED on the operator's screen.
T+60 s  |  ±1–2 m
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// LAUNCH KINETICS

Two launcher
configurations

LAUNCH PARAMETERS
4–6 bar
working CO₂ pressure
~0.1 s
acceleration in tube
Initial speed90 km/h
Launch G-force~27g
Configuration Aclosed tube
Configuration Bhandheld rail
Drone mass (with battery)~560 g
Launch prep time<30 s
SOLENOID CO₂ 6L TRG DRONE / FOLDED 0–75° L = 1200 mm Ø130 mm Ø150 1 2 3 4 5 6 SPECIFICATION 1 — Al BARREL 1200mm 2 — 24VDC VALVE 3 — CO₂ TANK 6L 4 — PIVOT JOINT 5 — DRONE 560g (FOLDED) 6 — TRIGGER PRES: 4–6 BAR CO₂ LAUNCHER PNEUMATIC LAUNCHER SECTION A-A / SIDE VIEW SCALE: NTS MAT: Al 6061 / CF SYSTEM MASS: ~7.5 kg ЧЕ-001 REV A DATE: 2026 OrbEye v1.0 CONFIGURATION B HANDHELD RAIL / CONCEPT SIDE VIEW LAUNCH VECTOR RAIL CARRIAGE DRONE SCREEN POWER MODULE 1 2 3 SPECIFICATION 1 — OPEN RAIL 2 — DRONE ON CARRIAGE 3 — CAPTURE SCREEN
The launch system design is selected based on the carrier and application conditions: manual operator, helicopter board, boat, or jet ski.
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300m 200m 100m 0m 0 20s 40s 60s LAUNCH 0–3 s CRUISE 3–55 s DESTROYED 55–60 s ◀ 5 m 90 km/h 85 km/h 5 m/s TIME ALTITUDE
// FLIGHT TRAJECTORY

Three phases.
One result.

01 — LAUNCH
Pneumatic ejection at calculated angle. Initial speed 90 km/h. Motors take control 0.5 s after exiting the tube.
02 — CRUISE
Onboard ieveraging AI and computer vision tracks the selected object via video stream. Autopilot maintains course, speed, and altitude using IMU + barometer data.
03 — DESTROYED
Computer Vision. Terminal guidance. Warhead initiation. Target Destroyed. Status OBJECT_DESTROYED on the launcher screen.
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// TARGETING SYSTEM

SCREEN → ieveraging AI and computer vision →
DESTROYED

STAGE 1 — SCREEN LOCK
Operator selects object on the launcher screen. The system transmits the visual target to the onboard ieveraging AI and computer vision and launches the mission.
STAGE 2 — COMPUTER VISION
RPi Zero 2W + Coral USB Accelerator (Edge TPU, 30+ FPS). YOLO — object detection; Optical Flow — tracking and stabilization. Course correction is performed inside the drone based on the video stream.
STAGE 3 — OBJECT DESTROYED
Terminal phase. Instant detonation at the point of contact. The launcher screen displays the status OBJECT_DESTROYED.
20 m 10 m 5 m DESTROYED ACCURACY: ±1–2 M ieveraging AI and computer vision
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// TABLE: DISTANCE / TIME

Calculation of flight time
based on distance to the object

Distance Time Phase Accuracy
100 m ~12 s LAUNCH→DESTROYED ±1–2 m
250 m ~22 s LAUNCH→CRUISE→DESTROYED ±1–2 m
500 m ~36 s LAUNCH→CRUISE→DESTROYED ±1–2 m
750 m ~48 s LAUNCH→CRUISE→DESTROYED ±1–2 m
1000 m ≤60 s LAUNCH→CRUISE→DESTROYED ±1–2 m
* Calculation: v₀ = 90 km/h = 25 m/s (a=27g, t=0.1s), cruise ≈ 75–85 km/h.
DESTROYED phase ≈ 10 s (Coral USB, YOLO + Optical Flow). Conservative estimate.
0s 30s 50s 60s 100m 250m 500m 750m 1 km 12s 22s 36s 48s 60s
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// HARDWARE PLATFORM

FPV-platform.
Fast. Reliable.

Based on a proven 5" racing platform, adapted for autonomous flight. Serviced in the field in 10 minutes.
KEY COMPONENTS
Frame5" True-X, carbon fiber CF 3 mm
Flight controllerPixhawk 6C / ArduPilot
Motors2306 2450KV × 4
ESC45A BLHeli32 4-in-1
Capture screenin the launcher
Companion ComputerRPi Zero 2W + Coral USB Acc.
Ieveraging AI and computer vision cameraOV5647 / Wide FOV 62°
Battery4S 1500 mAh LiPo
FRONT VIEW TOP VIEW SIDE VIEW 4S LiPo 220 mm (WB) H=160 PIXHAWK ArduPilot RPi CW CCW CCW CW SCREEN Ieveraging AI and computer vision/OV5647 220 mm LINK 4S LiPo CG ~160mm ORBEYE DRONE v1.0 ЧЕ-002 REV A / 2026 3-VIEW DRAWING MASS: ~560 g (w/ BAT) SPAN: 220 mm WB FRAME: 5" CF True-X HEIGHT: ~160 mm MOTOR: 2306 2450KV ×4 ESC: 45A BLHeli32 4-in-1 FC: PIXHAWK 6C BAT: 4S 1500 mAh LiPo SCREEN: TARGET DESTROYED COMP: RPi Zero 2W Ieveraging AI and computer vision: Coral USB (30+ FPS) THRUST: ~3400g TWR 6:1
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// TACTICAL AND TECHNICAL SPECIFICATIONS

Specification OrbEye v1.0

FLIGHT PARAMETERS
Max range1000 m
Time to position≤60 s
Initial speed (launch)90 km/h
Cruising speed85 km/h
Hover~4–5 min (in calm)
Working altitude30–150 m AGL*
Wind resistanceup to 12 m/s
POSITIONING ACCURACY
Target DESTROYEDlauncher screen
Ieveraging AI and computer vision tracking±1–2 m
Hover stabilization±0.3–0.8 m
Final distance5 m
DESTROYED phase time~10 s (Coral USB)
AutopilotArduPilot AUTO/LOITER
LAUNCH SYSTEM
Launch typePneumatic CO₂
Launch carriersground / helicopter / jet ski
Modessemi-auto with operator / auto
Working pressure4–6 bar CO₂
Tube length1.2 m
G-force / time~27g / ~0.1 s
Launch angle15° – 75°
Preparation<30 s
System mass~8 kg (with drone)
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// TEST LOG

Launches.
Real data.

A series of test launches at approved open sites (field, proving ground). Every launch is logged via MAVLink telemetry. Result: LOCK is consistently achieved in winds up to 8 m/s.
12
launches
total conducted
100%
success
LOCK achieved
47
s avg.
average LOCK time
#DistanceWindTimeResult
01120 m2 m/s14 sDESTROYED ✓
02250 m3 m/s24 sDESTROYED ✓
03250 m7 m/s29 sDESTROYED ✓
04500 m4 m/s38 sDESTROYED ✓
05500 m8 m/s44 sDESTROYED ✓
06750 m5 m/s51 sDESTROYED ✓
07 980 m 6 m/s 58 s DESTROYED ✓
Launches 08–12: re-validation at distances 100–500 m under various lighting conditions.
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// LAUNCHER SCREEN

Operator selects the object.
Onboard ieveraging AI and computer vision does the rest.

LAUNCH SCREEN operator points out object on video ONBOARD ieveraging AI and computer vision lock and tracking ≤60 s OBJECT LOCKED 5 m / ±1–2 m / VIDEO OPERATOR SCREEN strike status, elimination frame
CAPTURE INTERFACE
On the launcher screen, the operator marks the object directly on the video stream.
After launch, the drone autonomously tracks the target using onboard ieveraging AI and computer vision and returns the status OBJECT_LOCKED.
WHAT THE OPERATOR SEES
Combat mode activated. Drone on attack course. The screen displays targeting parameters, warhead status, kill probability, and readiness for final strike. Autonomous destruction without external command.
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// COST CALCULATION

Small batch.
Components estimate.

Engineering estimate for a batch after a series of test launches.
FPV frame + electronics
5" carbon, 4× 2306, 45A ESC, Pixhawk 6C
$850–1350
Capture screen + telemetry
Launcher display, video link, radio channel
$180–320
Companion Computer + ieveraging AI and computer vision
RPi Zero 2W, Coral USB Acc. (Edge TPU), OV5647
$450–800
Pneumatic launcher
Tube / rail, power module, capture screen, housing
$700–1400
Batteries + Charger
2× 4S 1500 mAh + balance charger
$220–380
Other (fasteners, cables, housing)
Printed parts, wires, terminals
$180–350
TOTAL small batch $2580–4600
SERIAL UNIT
Drone (components)~$900
Launch system~$650
Software and calibrationincluded in series
Serial unit ~$1850/unit
LAUNCH COST (service)
Deployment + setup + 1–3 launches + OBJECT_LOCKED.
Target price per event:
$2500–6000
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// NEXT STEP

Contacts us
at your facility.

We are ready to cooperate in the field of pilot production at an industrial site for testing, adaptation, and scaling. launch in a convenient location: from the ground, by helicopter, or by jet ski. Full cycle: AIM → LAUNCH → TRACK → DESTROYED — in semi-automatic or automatic mode, at an agreed distance up to 500 m.
CONTACT
OrbEye Team
Two engineers. One protocol.
hello@orbeye.one
Ready for a partnership in pilot manufacturing on an industrial site for testing, adaptation, and scale-up.
Location: Dubai / region
Demo: approved proving ground
OrbEye v1.0 CONCEPT BRIEF  |  CONFIDENTIAL  |  2026
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