1:1 simulated cockpit
Semi-closed instructor ""♠↕operation station (2₩£₩£ touch-screen)
GARMIN Perspective+ (P♥↓≤✘FD & MFD)
GFC700 Auto Pilot System
Closed-loop control loading sy✘π¥stem
Electrical pitch and roll trim
VSV HD 3 Channel Visual System
Using a fully self-developed p ↕∑rofessional flight simulation platform,βδ'& with a complete aerodyna©∏mic model and engine mode§l. Higher iteration frequency and¶λ§€ faster speed.
A self-developed data collection systeσπ•βm, with flight test da÷♦ta and engineering calcul↔γation data as data sources, based o§•n a self-developed data package of ↕δflight test data.
The aerodynamic model inc★ σludes subjects outside the flight envΩ©£elope (such as stall, spiral©★, etc.).
The simulation level is higher than th§"e requirements of FTD5, wh♦σ←ich can demonstrate individu↑<←£al characteristics specif ≥≥ic to specific aircraft ≤€models.
The avionics simφ ulation system is self-developed ≠by U-Wing, and it is stable and reliab™∞le under Linux operating system.；
The simulation hardware i☆ $ s the same as the real aircraft, w♣Ωith high reliability and low mα↑λaintenance cost；
Independently developed G1000 NXi, G×π♥3X, G660 and G5 avionics si ₹φ€mulation systems, fully covering the Ω'♦functions of aviation sc♣α₩hool training subjec✔±δts;
The navigation databas≠↑α'e is accurate and does not need to ©≈λbe calibrated one by one.
Self-developed IOS Sy∞™ ↔stem, and the softwarσ↕∑e interface is user-friendl"✘y and customizable (ad£↕¶vanced computer skills ar÷✘e not required).
Equipped with flight training rec→βording, playback, and ♣∑<evaluation functions, he∑εlping trainees improve t→↓♣☆raining effectiveness more eff∑✘iciently.
U-WING adopts the VSV visua αl system that is most suitab$↔le for general aviation air↓×αcraft. By combining high-precisio→λ n satellite data with large-scale au∞β®βtomatic 3D modeling technology™∞₹, it meets the customized requir™±ements of high-precisi β✔∏on urban visual simulat★₹↕$ion, especially the pre∑✘€cise modeling of landmark b¥<uildings. It is more in line with≤¶ the characteristics of visual flighδε±t at low altitudes for general∑★ aviation aircraft. It☆→↓© has won the first prize of Nati±₽£onal Science and Technology Progr♦≠εess Award.
