CKS-313T1 test and control radio station


The CKS-313T1 telemetry and control station can be used as an airborne station or a ground station. It establishes a wireless communication link between the airborne station and the ground station, and then uploads and downloads data according to the predetermined time sequence logic. It also has the capability to communicate with multiple airborne stations from one ground station (it can connect up to 20 airborne stations).
CKS-313T1 test and control radio station

Technical Parameters


Maximum range Greater than 300km (line of sight)
Power supply 28V DC
Communication interface RS422 1 channel
Discrete output 6 channels
Interface baud rate 115.2kbps
Maximum range Greater than 300km (line of sight)
Data update rate 20Hz
Carrier frequency 405MHz-415MHz frequency hopping/fixed frequency
Transmit power 20W
Receive sensitivity -121dbm
Operating temperature -55℃~85℃(﹣40℃ startup,﹣55℃ operation)
Storage temperature ﹣40℃~﹢65℃
Shock 15g

The CKS-313T1 telemetry radio can be used as an airborne station or a ground station. It establishes a wireless communication link between the airborne station and the ground station, and then uploads and downloads data according to the predetermined time sequence logic. It also has the capability to communicate with multiple airborne stations from one ground station (it can connect up to 20 airborne stations).

Other Content


CKS-313T2 control station

The CKS-313T2 dual-frequency telemetry and control transceiver can be used as an airborne unit or ground station. It establishes a wireless communication link between the airborne unit and the ground station, then uploads and downloads data according to a predetermined time sequence logic. The dual-frequency telemetry and control architecture can handle emergencies; when one channel fails, the other can be used as a backup. It also has the capability to communicate with multiple airborne units from one ground station (up to 20 airborne units can be connected).

KFS-3B integrated control and navigation unit

The KFS-3B flight control and navigation unit consists of a MEMS inertial measurement unit, a GNSS receiver, an atmospheric pressure sensor, and a main controller based on a high-performance ARM. The flight control and navigation unit uses sensor measurements to determine the flight path and commands, performing real-time calculations and controlling the aircraft to achieve flight control and navigation. It uses a MEMS inertial measurement unit to measure and collect the carrier's raw inertial navigation data, including rate gyro data and accelerometer data. A GNSS receiver obtains GNSS position and velocity data; dual GNSS is used to improve performance and reliability. An atmospheric pressure sensor receives total and static pressure from the airspeed tube to calculate parameters such as true airspeed, indicated airspeed, and flight altitude. Inertial navigation and GNSS combined navigation calculations are performed, and then the aircraft's control surfaces are controlled to achieve climbing, descending, and turning.

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