S40U Flight controller, Hybrid UAV Flight Control and Navigation System

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Description

The S40U flight controller and navigation system is suitable for small conventional electric or oil-powered fixed-wing, vertical take-off and landing fixed-wing, multi-rotor and other layout aircraft. It integrates a flight control for drone computer and a high-precision, high-dynamic micro-combined navigation system (BD/GPS/MINS, built-in domestic satellite navigation board, support BD2/BD3 priority), supports RTK high-precision positioning and dual-antenna high-precision direction finding, and can realize one-button automatic take-off, landing, hovering, circling, returning, setting altitude, parachute opening and various forms of autonomous cruising according to the predetermined route.

S40U supports four layouts of UAVs (including the conventional tail, V-tail, and flying wing): electric and hydraulic (vertical takeoff and landing fixed wing), conventional fixed-wing, tilt-rotor, and multi-rotor. There is also an integrated micro GPS/MINS navigation system, barometric altimeter, differential pressure airspeed meter, 2-channel speed measurement, and 1-channel fuel quantity measurement.

Up to 100 emergency landing points can be preset, and in case of emergency protection, it will automatically land at the nearest location. The system provides 8 user routes, each route can add 800 waypoints, automatically generates circling routes, circling center, and circling radius, and the number of circling circles can be set

S40U provides photo capturing (shutter control) tasks during the flight paths, and the timing/distance can be set. It also supports typical photoelectric pod, pan/tilt gimbals, and special surveying and mapping cameras. Flight information and mission information are recorded and downloaded separately. The flight information recording time is up to 9 hours.

A ground measurement and control software supports online maps and irregular multi-measurement area automatic surveying and mapping route planning, supports automatic planning of oil, electric power, and other patrol routes, and can alert users to complete pre-flight planning examinations.

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If you have any questions regarding our products, use the Motionew Contact us page to consult our engineering team.

 

Specifications

Attitude accuracy 0.3°
Heading accuracy
0.1° (dual antenna, 2m baseline)
0.2° (1m baseline)
0.3° (single antenna, need to maneuver)
Positioning accuracy

Single point positioning: 1.5m
RTK: 0.8cm
Angular velocity measurement range ±500°/s
Acceleration measurement range ±8g
Height measuring range 10000m
Voltage monitoring range 0~52v
Servo update frequency 50Hz
Engine speed monitoring range 0~20000rpm
Communication Interface RS-232C
Voltage monitoring channel 2
Engine rotation monitoring channel 2
PWM control channel 9
Digital output channel 3 (configurable as PWM)
Extended serial port 3 (can be connected to payload, etc.)
SBUS input channel 1
Number of routes 8 routes (800 waypoints per route)
Built-in data logger 9 hours
Position Points for taking pictures 10000
Emergency landing point 100
Supply voltage 4.5 v- 9v
Power Consumption < 3.5W
Weight 150g
Dimensions 109x56x32.5mm
Operating Temperature -40°C~55°C
Storage Temperature -40°C~85°C

Product contents

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Documents

 

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