Diamond DA40 Full Motion Simulator

Overview

Experience Subject

  • Normal Flight Standard Operating Procedure (SOP) 

  • VFR Circuit Base Training 

  • IFR Training 

  • Complex weather flight training

  • Aircraft main failures and special condition training 

  • Extreme Flight training course

  • Other supplementary subjects

Flight simulation system

Using a fully self-developed professional flight simulation platform, with a complete aerodynamic model and engine model. Higher iteration frequency and faster speed.

A self-developed data collection system, with flight test data and engineering calculation data as data sources, based on a self-developed data package of flight test data.

The aerodynamic model includes subjects outside the flight envelope (such as stall, spiral, etc).

Avionics system

The  avionics simulation system is self-developed by U-Wing, and it is stable and reliable under Linux operating system. 

The simulation hardware is the same as the real aircraft, with high reliability and low maintenance cost;

Independently developed G1000 NXi, G3X, G660 and G5 avionics simulation systems, fully covering the functions of aviation school training subjects.

The navigation database is accurate and does not need to be calibrated one by one.

Instructor control system

The self-developed instructor operating system has an easy-to-use software interface that can be customized, and does not require advanced computer skills to deliver excellent training. 

It features flight training recording, playback, and review functions to help students improve their training more efficiently.

Visual system

U-WING adopts the VSV visual system that is most suitable for general aviation aircraft. By combining high-precision satellite data with large-scale automatic 3D modeling technology, it meets the customized requirements of high-precision urban visual simulation, especially the precise modeling of landmark buildings. It is more in line with the characteristics of visual flight at low altitudes for general aviation aircraft. It has won the first prize of National Science and Technology Progress Award.

Technical parameters
Size(mm)
2644×2200×2646

Power(KW)
5

Voltage(V)
220

Temperature(°C)
5-33

Humidity(%rh)
≤75

Weight(KG)
300-700