FLIGHT CONTROL SYSTEM

It’s a servo motor required for aircrafts to fly by changing angle of propeller/rotor such as controllable-pitch multicopter and single helicopter.
Readily available as long as it is a PWM output compatible servo motor (up to 400 Hz).

It’s a wireless device to control an aircraft.
It is compatible with transceiver corresponding to S.BUS of Futaba Corporation and that of TKK Works.

For such an accident of crash, calculation results of flight are recorded in order to identify cause of the crash.
The data is surely retained even in a case that power was lost at a time of crash or battery was about to out of charge in the sky.

It’s a radio unit to transmit data of conditions of aircraft including flight equipment and flight speed to the ground.
It is possible to install a radio unit with frequency band of 2.4 GHz which is not required for a license and long distance radio by selecting a public radio such as LTEs.
It is also possible to transmit real time information with a frequency of 100 Hz by using a radio unit with a transfer capability of 160 kbps.

It’s a servo motor required for aircrafts to fly by changing angle of propeller/rotor such as controllable-pitch multicopter and single helicopter.
Readily available as long as it is a PWM output compatible servo motor (up to 400 Hz).

Flight controller with domestic original hardware and software.
With leading-edge technology and engineering as well as repeated flight tests, it has been produced to be able to control aircrafts with various shapes. In addition, simple flight.

It’s a servo motor required for aircrafts to fly by changing angle of propeller/rotor such as controllable-pitch multicopter and single helicopter.
Readily available as long as it is a PWM output compatible servo motor (up to 400 Hz).

It is a device to measure distance between the aircraft and the ground during flight.
With a capability to measure distance of about 100 m, measurement results are available as supportive information for flight at the time of landing and low-altitude flight.

It’s a device to forcibly bring down the aircraft when it lost its control.
It is also possible to interlock with a parachute deployment signal optionally.

It’s an inertial measurement sensor which is most important for flight. The sensor is equipped with functions of a sensor of acceleration, gyro, pressure and geomagnetism as well as of a GNSS receiver.
It is possible to measure acceleration and angular rate, attitude angle, speed, position and altitude at the same time with this sensor alone.

A unit of both large-sized motor and ESC is mounted on aircrafts such as our original controllable-pitch multicopter and single rotor helicopter.
For ordinary aircrafts such as fixed pitch multicopter, small-sized motors and ESCs are mounted by a number of the arms.
Our flight control system is capable of mounting up to 8 units (8ch) of ESCs and motors each regardless of the size of aircrafts (mounting of more than 8 units is also available optionally).

A unit of both large-sized motor and ESC is mounted on aircrafts such as our original controllable-pitch multicopter and single rotor helicopter.
For ordinary aircrafts such as fixed pitch multicopter, small-sized motors and ESCs are mounted by a number of the arms.
Our flight control system is capable of mounting up to 8 units (8ch) of ESCs and motors each regardless of the size of aircrafts (mounting of more than 8 units is also available optionally).

It uses an antenna compatible with “Michibiki”, a GNSS satellite of Japan.
Installing position is considered not to receive incorrect radio wave called multipath.

It’s a servo motor required for aircrafts to fly by changing angle of propeller/rotor such as controllable-pitch multicopter and single helicopter.
Readily available as long as it is a PWM output compatible servo motor (up to 400 Hz).