UAV Core Components
Integrated Portfolio
Electro-Optics · Flight Control · Solid-State Power · Propulsion
Four core subsystems engineered for uncrewed platforms — from loitering munitions and target drones to high-speed UAVs and R&D flight-test vehicles.
EO / Night Vision Pod
Intelligent Flight Controller
Solid-state Battery
Turbojet Engine
01 Loitering Munition / UAV EO Night Vision System
Product Overview
Designed exclusively for loitering munitions, the XY-201-132-60 pod integrates advanced full-colour night vision technology. It achieves precise target capture at long distances after dark and overcomes the defects of traditional night vision and AI recognition systems. It enables round-the-clock missions and greatly improves the overall combat effectiveness of loitering munitions.
Technical Specifications
Subsystem
Parameter
Specification
All-colour Night Vision
Resolution & pixel size
1920 × 1080 @ 2.9 μm
Focal length
12 mm
Electronic zoom
1× / 2× / 3× / 4× / 5×
Minimum colour illuminance
0.001 lux
Minimum monochrome illuminance
0.0005 lux
Detection range (4 m × 6 m target)
5,000 m
Recognition range (4 m × 6 m target)
≥ 1,000 m
Field of view (H × V)
≥ 48° × 26°
Thermal Imaging
Resolution & pixel size
640 × 512 @ 12 μm
Focal length
13 mm
Recognition range (4 m × 6 m target)
≥ 500 m
Field of view (H × V)
≥ 25° × 15°
2-Axis Turret
Azimuth range
−115° to +115°
Pitch range
−80° to +15°
Line-of-sight stabilisation accuracy
≤ 3 mrad (RMS)
Physical Size & Weight
Dimension (L × W × H)
55 mm × 62 mm × 82 mm
Weight
300 g
02 Intelligent Flight Controller
High-Precision · Multi-Redundant · GNSS-Denied Capable · AI-Enabled Autopilot for Industrial UAVs
Conventional autopilots lose their way when GNSS is jammed, spoofed, or unavailable. The F-Series doesn’t. It combines a triple-redundant industrial sensor core with centimetre-level RTK, adds GNSS-denied visual navigation (F300 heritage) and a dual-redundant anti-jamming / anti-spoofing architecture (F500 heritage) — then layers on AI visual recognition and swarm coordination. Your platform knows where it is, sees what it needs to see, and flies as one with the fleet. Small enough to fit anywhere — 147 g. Robust enough to go anywhere — −40°C to +85°C.
AI Recognition & Precision Engagement
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Marker-based precision landing — QR-code recognition fused with a high-precision control model for reliable point-to-point landing in complex environments: logistics last-metre delivery, dock / nest recovery, emergency ops, fixed-point inspection cycles.
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Visual target guidance — vision-based target cueing for both fixed-wing and multi-rotor platforms, plus GNSS-based target guidance.
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Visual tracking — real-time dynamic tracking flight; precision guidance against both static and moving targets.
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Precision airdrop — high-accuracy route positioning for pinpoint payload release.
Result:
the aircraft doesn’t just reach the coordinate — it identifies the target and closes on it.
Swarm & Formation
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Multi-rotor swarm mode — coordinated flight with efficient collaboration and adaptive response.
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Leader-follower architecture — configurable vehicle IDs with follow-enable; a single primary mesh link is enough to put the whole fleet into coordinated flight.
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Proven at scale — VTOL fixed-wing swarm operations delivered to customers (15-aircraft coordinated missions).
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Intelligent wind rejection — multi-rotor smart wind compensation keeps formation stable in complex airflow.
Result:
one operator, many aircraft, one coherent mission.
Core Capabilities
Capability
What it delivers
Triple-redundant sensors
3× accel + 3× gyro, real-time health monitoring, automatic seamless fail-over
GNSS-denied navigation
Full navigation with visual module; heading self-alignment; built for low-altitude penetration & long-range missions
Anti-jamming / anti-spoofing
Dual-redundant, mutually backed-up navigation sources — “double insurance”
AI visual recognition
QR-code / marker recognition + visual target detection, guidance and tracking
Swarm & formation
Multi-rotor swarm flight, leader-follower, coordinated multi-vehicle missions
Centimetre-level RTK
0.8 cm + 1 ppm horizontal / 1.5 cm + 1 ppm vertical
Aerospace-grade interconnect
J30J metal-shielded connectors — anti-interference, shock-resistant
40+ interfaces
16 PWM · 2 CAN · S.Bus · 2 I2C · 6 serial (1 RS232 + 5 TTL) · 3 voltage monitoring
03 Solid-State UAV Battery
Materials & electrolyte research.
Our solid-state electrolyte is formulated in-house, not licensed in — letting us balance energy density, rate capability and cycle life ourselves.
Interface & cell architecture.
Performance in solid-state cells is won at the electrode–electrolyte interface. We engineer interfacial stability and stack architecture so gains survive real discharge profiles.
Thermal & environmental.
Cells hold performance across a 105-degree span, with no external heating or active cooling.
Duty-cycle & lifecycle.
Designed around a practical operating window, not a laboratory maximum — shallower discharge yields more lifetime energy throughput.
Our solid-state platform is developed end to end — electrolyte formulation, electrode system, cell architecture and validation — inside our own laboratories.
Key Specifications
Parameter
LV-AF500-1
Nominal capacity (C/10, 25°C)
8,000 mAh
Nominal voltage / range
3.8 V / 3.0 – 4.5 V
Energy density
>450 Wh/kg · >1,000 Wh/L
Continuous discharge rate
7C
Weight
~70 g
Dimensions (L × W × T)
80 × 70 × 6.5 mm
Operating temperature
−40°C to +65°C
Cycle life
~320 cycles @ 100% DoD · ~500 cycles @ ≤ 80% DoD
04 UAV Turbojet Engine
Our solid-state platform is developed end to end — electrolyte formulation, electrode system, cell architecture and validation — inside our own laboratories.
Full-spectrum thrust coverage.
One supplier from 20 to 250 kgf — scale your platform without changing your engine partner.
Class-leading fuel economy.
Specific fuel consumption drops from 1.75 to 1.25 kg/(kgf·h) as thrust rises; the WP250 is the most efficient engine in the range.
High-altitude, high-subsonic performance.
Operates up to 13,000 m and Mach 0.95, meeting the demands of modern high-speed target and missile applications.
Compact, airframe-friendly packaging.
Diameters from 115 mm and lengths from 300 mm — minimal drag, easy fuselage integration.
Dependable starting.
Electric start across the family; the WP20 additionally supports cartridge (cannon) start for rapid, infrastructure-free launch.
Product Family
Model
Thrust (kgf)
Dimensions D × L (mm)
SFC kg/(kgf·h)
Max. operating altitude (m)
Operating Mach No.
Starting method
WP20
20
115 × 300
1.75
8,000
0 – 0.70
Electric / cartridge (cannon) start
WP50
50
150 × 380
1.50
10,000
0 – 0.80
Electric start
WP90
90
204 × 480
1.38
12,000
0 – 0.90
Electric start
WP120
120
240 × 515
1.28
12,000
0 – 0.90
Electric start
WP250
250
320 × 650
1.25
13,000
0 – 0.95
Electric start
Applications
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Target drones
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Target missiles
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Loitering munitions
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Decoys
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High-speed UAVs
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R&D and flight-test platforms