AGRI 1900
AGRI 1900
- Autonomous and Remotely Piloted Flight
- Real-Time Data Link
- Flight Data Management System
- Wireless Video Capabilities
- Data Logging and Telemetry
The AGRI-1900 is designed for precision farming and territorial monitoring, offering real-time interaction with ground control. It provides flexibility with reduced cost and risk, featuring a flight control system for automatic stability, guidance, and navigation.
The AGRI-1900 has a fixed wing, T-tail configuration, known for its payload capabilities and flight performance. It is easy to launch, light, compact, and aerodynamically efficient, with smooth stall and stable flight characteristics.
MAVTechs.r.l., a spin-off of Politecnico di Torino, is a certified RPAS Consultant Organization. The company focuses on innovative aeronautical solutions for civil applications, including the design and production of RPAS and integration with customer applications.
- Take off: Hand launch or catapult assisted
- Recovery: Autonomous or radio-controlled landing, optional emergency parachute
- Operating altitude: 150 m a.g.l.
- Maximum wind intensity: 20 km/h
- Rain tolerance: Light rain
- Transport: Breakdown into a rigid case
- Power: Li-Po battery, brushless DC electric motor
- RC receiver range: 2000 m (line of sight)
- Video transmission range: >300 m (line of sight)
- Autopilot: Programmable waypoint sequence
- Data-logging and telemetry via radio-modem
- Construction: EPO
- Wingspan: 1900 mm
- Weight: < 2500 g
- Payload: < 300 g
- Airspeed: 7.5 ÷ 20 m/s
- Range: 250 m ÷ 7500 m
- Endurance: 30 min @ 12.5 m/s
Catalog excerpts
Remotely Piloted Aircraft System Description Features Autonomous and Remotely Piloted Flight The AGRI-1900 Remotely Piloted Aircraft System has been developed in order to perform data acquisition for precision farming and territorial monitoring, allowing a full interaction with ground control through a real time up and down data link with the aircraft. The advantage of using scaled RPAS platforms is the flexibility with reduced cost and risk. A flight control system (providing automatic stability, guidance and navigation capabilities) is installed on the vehicle and the flight parameters can be evaluated in real time or in post-flight mode. Real-Time “Up and Down” Data Link Flight Data Management System Wireless Video Capabilities Data Logging an
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Application Outline Company Profile Take off: hand launch or catapult assisted. Recovery: autonomous or radio controlled landing or emergency parachute drop (optional). Operating altitude (typical): 150 m a.g.l.. The maximum adverse wind intensity for regular flight is 20 km/h. Rain tolerance: light rain only. Transport: breakdown into a rigid case. Onboard voltage supplied by a Li-Po sealed battery pack. Propulsion: high performance brushless DC electric motor with pusher propeller. RC receiver range for pilot in command mode (2.4 GHz in-flight manual override): 2000 m (line of sight). Standard...
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