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Who we are

AUTOLAND.UAS, founded in 1990, is a trusted leader in automation systems across Japan, Europe, and the U.S.
In 2025, we advance into next-generation aerospace with military-grade, modular, and fully customizable commercial drone platforms.
AUTOLAND.UAS is driving the future of intelligent, mission-ready flight.

Core Competence

Technology-Driven Solutions

About Autoland.uas , we leverage our accumulated experience in automation systems to swiftly develop application systems tailored to diverse needs, in collaboration with various drone manufacturers.

All-in-One System Integration
We provide complete UAV integration—from airframe and flight control to sensors, communication, and ground control. Custom payloads can be quickly deployed for various mission needs.

Highly Customizable & Secure
Platforms are tailored to specific use cases with custom airframe and payload design. All core components are Made in Taiwan, ensuring high data security standards for government and enterprise use.

Defense & Commercial Applications

Defense: ISR missions, aerial support, tactical training, and target drone systems
Commercial: Infrastructure inspection, agriculture, smart city surveillance, and emergency logistics

Global Expansion with Strong Industry Alliances
With the backing of Tung Chien An Automation, we partner across industries to accelerate deployment and scale UAV solutions globally.

Our Services

Airframe Design & Manufacturing

Design of medium to large UAV structures (Fixed-wing / VTOL / Target drones / Loitering munitions / Rotorcraft)
Custom selection of materials including carbon fiber, aluminum alloys, and advanced composites

Flight Control &

Navigation System Development

In-house development of autonomous flight controllers (supports high-wind operation and anti-interference)
Sensor fusion algorithm integrating optical flow + GPS + LiDAR + barometric data
High-precision AHRS (Attitude and Heading Reference System)
Centimeter-level hovering and precision path control

Integrated UAV Solutions

Mission-specific UAV development tailored to client projects
Modular vehicle and mission payload designs (e.g. mapping, surveillance, armed, spraying, etc.)
Seamless API integration between mission computer and flight control system
Integration with industrial/military-grade communication systems (UHF, 5G, satellite links)

Ground Control &

Backend Support

Ground Control Station (GCS) design and integration (compatible with Windows / Linux)
Remote control development supporting LabVIEW API / UART interfaces
Remote UAV operation, mission monitoring, and flight path logging systems
Ground system integration (MIS, data transmission, cloud platform support)

Testing &

Regulatory Compliance

Full-process flight testing services (functionality, wind resistance, payload capacity, endurance, etc.)
Implementation of flight data logging and mission playback features

Technical Consulting &

Project Collaboration

Customized mission evaluation and UAV implementation consulting
Collaborative development projects with enterprises, research institutions, and governments (CDMO model)
Overseas market entry consultation and localization partnership strategies

UNMANNED AERIAL VEHICLE PLATFORM

AL-200 FIXED-WING UAV

Specializes in long-range, heavy-payload UAVs with military-grade technology and advanced mission customization.

Extended Endurance
Up to 10 hours flight time with optimized payload ratio.

Heavy Payload
Carries up to 50 kg; supports EO/IR sensors and mission equipment.

High Altitude
Operates up to 2,000 meters, fit for varied terrains and missions.

Custom Design
High-wing pusher design for stability, flexibility, and integration.

Powerful Engine
35–38 HP output supports heavy loads and high-power tasks.

Long-Range Control
Multi-channel datalink with directional antenna, range 150 km.

1/1

AL-200

Wing Span
Overall Length
Overall Height
Net Weight

Propulsion

Max payload
Max takeoff Weight

835cm
410cm
110cm
100kg
35~38hp

2stroke gasoline engine
50kg
200kg

Max Level Speed
Operational Altitude
Cruising Speed
Endurance
Operating Range
Take off Method
Recover Method
Body material

130 km/h
2,000m
110 km/h
10hr at 100 km/h
150km
Runway
Runway
Composite Materials

TD-30

TD-30 TARGET DRONE

High-speed and realistic simulation—multi-role target drone designed for air-to-air weapon training.

Realistic Threat Simulation
Simulates various aerial targets—fighters, cruise missiles, and UAVs—to match complex threats faced by modern air defense systems.

Flexible Payload Integration
1.5 kg capacity with mounting points on wingtips, underwings, and fuselage for mission-specific payloads.

Customizable Support
Covers mission planning, flight control, tracking, data logging, and payload customization for air-defense training.

Cost-Effective Solution
Suitable for short-range and tactical missile system exercises.

1/1

Wing Span
Overall Length
Overall Height
Net Weight
Propulsion
Max Payload
Max take off Weight

200 cm
240 cm
50 cm
15kg
Jet engine 30kg
1.5 kg
30kg

Max Level Speed
Operational Altitude
Cruising Speed
Endurance
Operating Range
Take off Method
Recover Method
Body material

400 km/h
4,000m
180km/h
45min at 280km/h
150 km
Launch
Runway or parachute
Composite Materials

WPC-3K1
UNMANNED AERIAL VEHICLE PLATFORM

Highly agile and stable, with precision hovering and programmable control—built for inspection, surveillance, research, and defense applications.

Advanced Flight Control
Equipped with cutting-edge algorithms for 400Hz response and strong wind resistance (up to Beaufort scale 7–8), ensuring stable flight in harsh conditions.

High-Precision Positioning
Integrates GPS and optical flow sensing to achieve centimeter-level XY positioning, enabling accurate hovering and navigation in complex environments.

Accurate Altitude Control
Combines laser rangefinder and barometric altimeter for precise Z-axis management, ensuring consistent altitude and safe flight operations.

Precise Attitude Management
Utilizes an AHRS for high-precision attitude and heading control with excellent vibration resistance, improving flight stability and reliability.

Flexible Control Interface
UART interface supports both onboard mission computer and ground station control. Fully compatible with LabVIEW and Python APIs, allowing for programmable autonomy and enhanced integration flexibility.

Comprehensive Mission Logging
Built-in flight data recording (black box) for post-mission analysis, traceability, and performance optimization.

1/1

WPC-3K1

Wing Span
Overall Length
Overall Height
Net Weight
Propulsion
Max payload
Max takeoff Weight
Max Wind Speed Resistance
Hovering Accuracy Range

55cm
70cm
26.5cm
1.9kg
Battery & Motor
1kg
1kg
17.2 m/s
10cm

Endurance
Operating Range
Remote Control Comm Interface
SDK Communication Interface
Take off Method
Recover Method
Sensor Fusion Update Rate
Attitude Control Frequency
Flight Recorder
Body material

10-20min
3.4km
PWM
UART
VTOL
VTOL
400Hz
400Hz
USB
Carbon Fiber

Drone Development Process

Requirements Confirmation

Indoor / Outdoor Operation
Land / Maritime Reconnaissance
Mission Objectives
Control Altitude, Range, and Environmental Conditions

Aircraft Type Selection

Fixed-Wing UAV: High speed, long endurance, stable flight
Rotary-Wing UAV: Highly maneuverable, capable of hovering
VTOL (Vertical Take-Off and Landing):
No runway required for takeoff and landing

Specification Definition