Product

IAS500 Datalink

IAS500 is a highly integrated dual- serial datalink product with compact internal structure, unified power supply and data composite transmission, which is suitable for small and medium size unmanned systems. With internal P840, 1W power 840MHz micro datalink station of Canadian Microhard, it realizes data recombination through the internal integrated high- perfomanced CPU.

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DETAIL

IAS400 Datalink

IAS400 micro digital datalink, with ultra- small size and ultra- light weight, is an industrial level and highperformance wireless serial communication module for unmanned system- specific frequency ranges. It supports network, point- to- point and point- tomultipoint communication modes. The C11 operates at 840~845MHz and uses Frequency Hopping Spread Spectrum (FHSS) to achieve reliable wireless asynchronous data transmission.

DETAIL

IAS300 Datalink

IAS300 micro digital datalink is an industrial level and high- performance wireless serial communication module for unmanned system with specific frequency ranges. It supports network, point- to- point and point- to- multipoint communication modes. The C10 operates at 840~845MHz and uses Frequency Hopping Spread Spectrum (FHSS) to achieve reliable wireless asynchronous data transmission.

DETAIL

Differential Product

IAS200 product, integrated with differential satellite navigation system and datalink, is using compact internal structure, unified power supply and data composite transmission, and it is suitable for small size and medium size unmanned systems. With internal high precision GNSS receiver and 840MHz micro datalink station, it realizes data recombination with the internal integrated high- perfomanced CPU.

DETAIL

FC200 Flight Control

The FC200 series flight control and navigation system is designed for aircraft with miniature and small electric conventional fixed wing, vertical takeoff and landing fixed wing and tilting rotor layout. It is internally integrated with flight control computer, micro- integrated navigation system (GPS/MINS) , weighing only 85g.

DETAIL

FC300 Flight Control

The FC300 series, flight control and navigation system, is designed for an aircraft with miniature and small size electric conventional fixed- wing, vertical take- off and landing fixed- wing, also tilt- rotor layout. It is internally integrated with flight control computer, micro- integrated navigation system (GPS/MINS) and a datalink of 30km transmission distance, product's weight is only 95

DETAIL

FC400 Flight Control

The FC400 series (cost- effective), flight control and navigation system, is designed for small size conventional fixed- wing, vertical take- off and landing fixed- wing, tilt- rotor aircraft, with integrated flight control computer and micro- integrated navigation system (GPS/MINS). It is capable for one- key action, enabling automatic take- off and landing, hovering, circling, returning, altitude holding, parachute landing and various forms of autonomous cruise function according to the setting route. It provides a comprehensive flight status monitoring, alarm function and a comprehensive emergency protection mechanism to ensure the safe operation of the system.

DETAIL

FC400X Flight Control

The FC400X series, flight control and navigation system, is based on the S4 series. It is integrated with a wide range of temperature working sensors.The S4plus can stably work from - 40℃ to +85℃ .

DETAIL

FC500 Flight Control

The FC500 series (high precision), flight control and navigation system, is designed for small size and medium size conventional fixed- wing, vertical take- off and landing fixed- wing, tilt- rotor aircrafts. It is, with internal integrated flight control computer and tri- redundancy micro- integrated navigation systems (GPS/ MINS), capable for meeting the functions of one- key action to enable automatic take- off, landing, hovering, circling, returning, altitude holding, open a parachute landing and various forms of autonomous cruise function according to the required

DETAIL

FC600 Flight Control

FC600 series professional flight control and navigation system is suitable for large and medium- sized conventional fixed wing, vertical take- off and landing a fixed wing and layout of the tilt rotor aircraft. The internal integrated flight control computers and micro integrated navigation system (GPS/MINS) of triplex redundancy, can be a key to realization of fixed and mobile platform automatic take- off and landing, hover, hovering, high return, and open an umbrella and a variety of forms according to the scheduled routes cruise function independently.