Capability to control displacement:
Number of Degrees of freedom: 6 DOF
Maximum roll angle: ±22 degrees
Maximum pitch angle: ±22 degrees
Maximum yaw angle: ±22 degrees
Maximum vertical translation: ±35 cm
Maximum longitudinal translation: ±30 cm
Maximum lateral translation: ±40 cm
Load factor in direction X, Y, Z: 5 m/s2
Number of control states: 7
Communication period: ≤ 0.04 s
Process cycle: ≤ 0.04 s
Cycle of Display status update: ≤ 0.04 s
Type of Packaging data: Binary
Communication protocol: UDP/IP
Functions:
Convert analog input signals as accelerations, rotational angular, GPS information, etc. to digital and process those for subsequent calculations
Calculate longitudinal, lateral and vertical acceleration of helicopter to control the motion base
Calculate roll, pitch and yaw angle acceleration of helicopter to control the motion base
Process and Calculate rotational angular of helicopter to control the motion base
Calculate and optimize movement data of helicopter in order to make sure the motion base operates properly
Process and filter high order signals in order to give accuracy control information for the motion base
Create session with the motion base and process faults during connection
Maintain session with the motion base in order to communicate and control continuously
Control the motion base operation modes, include control base on platform accelerations or positions
Control the motion base in the platform accelerations mode
Control the motion base in the platform positions mode
Receive feedbacks of current platform attitudes and positions
Display current platform attitudes and positions and control information for users
Select motion base operating modes
Control motion base
Display the motion base status and information
Receive the motion base and helicopter information to synchronize and control both helicopter and motion base
Calculate and process flight dynamic data in order to generate effects as requirements
Calculate drag, lift and air brake forces to create appropriate effects for kinematics of helicopter
Integrate force effects into the simulation and manipulate them to create realistic motion experiences
Provide secondary effects such as vibration, fluctuation and deviation from fly track, increased and decreased altitude pressure
Monitor the artificial forces generation in order to operate safety for operators and facilities.
