High integrated and low-cost flight control & navigation system, applied for the micro and small full battery powered fixed wing UAV system.

Integrated professional IMU, magnetic sensor, dynamic and static pressure sensor and GPS module.

Support multiple auto takeoff mode of UAV, such as hand launch, catapult launching, vehicle assistant auto takeoff mode etc.

Support multiple recovery mode of UAV, such as parachute recovery, deep stall recovery and belly landing etc.

With adaptive control algorithm based on total energy, the normal configuration UAVs are ready to fly without parameters adjustments once autopilot installed.

Nonlinear high-accuracy GPS/SINS/AHRS fusion algorithm features the update frequency of 200Hz and automatic switching to AHRS mode smoothly to ensure flight safety in case of GPS loss.

Support customization fail-safe mechanisms request from end user, existing fail-safe mechanism are auto return by lower power, GPS lost, datalink timeout, RC command timeout, over limitation of altitude.

Support SBUS port for manually remote-control UAV.

Built-in 8Mbyte data recorder for 1-2 h flight logging data recording.

Built-in 1W FHSS telemetry radio module with communication range up to 60km.



Update frequency
10Hz,positioning accuracy 2.5m
3 axis gyroscopes
3 axis accelerator
Magnetic sensor
Static pressure sensor
15~115kPa,support 13000m
Dynamic pressure sensor
4kPa,support 280km/h
Integrated data link
Analogue input
1 channel, 12Bit
Communication interface
2channels RS232,1channel SBUS
Built-in data recorder
General I/O
8 channels, equipped PWM/IO/frequency input/output

Eiectric Specs

Power supply
Power consumption

Physical Specs


Operating Environment

Storage temperature
Operating temperature
Storage humidity
5% ~ 95%
Operating humidity
10% ~ 90%

*Actual product features and specifications (including but not limited to appearance, colour, and size), as well as actual display contents (including but not limited to backgrounds, interface, and icons) may vary by country. **All performance data in the foregoing pages are theoretical values obtained by JOUAV internal laboratories through tests carried out under particular conditions. For more information on the specific testing conditions, refer to the aforementioned product details. Actual performance may vary owing to differences in individual product configuration, software versions, application conditions, and environmental factors. All data is subject to actual usage. ***JOUAV makes every effort at the time of publication to ensure the accuracy of product information it provides. Due to subsequent changes involving product batches, production and supply factors, it may be necessary for JOUAV to make changes and adjustments to text and images so that they match the performance, specifications, indexes, and components of the actual product. Product information is subject to such changes and adjustments without notice. Any illegal utilization is forbidden as JOUAV series autopilots are sensitive items. Chengdu JOUAV Automation Tech Co., Ltd will not take any responsibility for any consequences caused by illegal use, nor provide any technical support or promise for any obtaining through irregular channels. We shall not be related to any third party liability by using the products.The direct or indirect application of JOUAV series autopilots and products will be considered as unconditional acceptance of this statement. If you have any dissent of any clauses, please immediately suspend the usage.

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