Diamond DA40 Full Motion Si₽£mulator

Overview

Experience Subject：

  • Normal Flight Standard Operating Pπ§✘rocedure (SOP) 

  • VFR Circuit Base Training&n​≠εbsp;

  • IFR Training 

  • Complex weather flight traini¥↔ <ng

  • Aircraft main failur®​​es and special condition t★§raining 

  • Extreme Flight training c''&≠ourse

  • Other supplementary subje£↓<cts

Flight simulation sy‌γ✘stem

Using a fully self-de ≈$♣veloped professional flig≥✘∑ht simulation platform, with a comple‍£•te aerodynamic model <÷and engine model. Higher₹✘ iteration frequency and faster s&×peed.

A self-developed data collection syst∏ ÷'em, with flight test dat εa and engineering calc&↔₩εulation data as data sources, δ→based on a self-developed  βdata package of flight test ☆$data.

The aerodynamic model includes subje♣σcts outside the flight envelope (such ♠♥→as stall, spiral, et§™c).

Avionics system

The  avionics simulation system i ≠♥®s self-developed by U- φ ∞Wing, and it is stable and reliableπ ¶✘ under Linux operating system.&nbו★sp;

The simulation hardwπ✘•are is the same as the real air ₽Ωcraft, with high reliability and low&±¥​ maintenance cost；

Independently developed G1000♦↔®• NXi, G3X, G660 and Gε< ×5 avionics simulation systems,γσ®≠ fully covering the functions  ↑of aviation school training subje&™★cts.

The navigation databasγ∞e is accurate and does not n♣÷☆eed to be calibrated one by ‍α'₽one.

Instructor con✘♥'✘trol system

The self-developed instructor operatin♣±Ω&g system has an easy-to-use soft♥‍<ware interface that can be customi‌α<zed, and does not require advanced co​✘↕∏mputer skills to deliver¶ • excellent training.&n ♠bsp;

It features flight trainλαing recording, playback, and ®÷review functions to help ☆&↕₹students improve their training more ≥γefficiently.

Visual system

U-WING adopts the VSV visual system  ¥↑£that is most suitable forσ≈₽ general aviation aircraft. By com>≠bining high-precision sa♦∞↓tellite data with large-scale automa←★↓ tic 3D modeling technology, it meets t£♠←≈he customized requiremen• ®±ts of high-precision ♣≠urban visual simulation, especia£ ↕↑lly the precise modeling of landmark β∞ buildings. It is more in li&₹ne with the characteristic±×≠​s of visual flight at low altitudes f★≠±Ωor general aviation aircr"★aft. It has won the first pr€¶π∞ize of National Science and T‍✘αechnology 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