Cirrus SR20 Level 5 FTD
1:1 simulated cockpitγ&
Semi-closed instruct♦♣©or operation station (2 toucλ♠Ω✔h-screen)
GARMIN Perspecti>÷ve+ (PFD & MFD)
GFC700 Auto Pilot Sys≠↑tem
Closed-loop control ↓loading system
Electrical pitch and roσ→∏★ll trim
VSV HD 3 Channel Visual System
Using a fully self-developed pro∑εfessional flight simulation plat®♣€form, with a complete aerodynamic model ₹®≥ and engine model. Higher iteration freσquency and faster speed.
A self-developed data collection system , with flight test data and engine∑'λering calculation data as d↕ ata sources, based on a self-developed φ±data package of flight test data.
The aerodynamic model includes s"φ≈ubjects outside the flight envelo↓≤±pe (such as stall, spiral, etc.).♦¥
The simulation level is higher t≠♣han the requirements ><of FTD5, which ca↔'<₹n demonstrate individual characteri∞× ↕stics specific to specific airc→∑raft models.
The avionics sim↓©ulation system is self-dev€←eloped by U-Wing, and it is✔§π₹ stable and reliable under Lin↔∞ux operating system.→✘βγ；
The simulation hardware is the s↔>≠Ωame as the real aircraft, w♦®&₹ith high reliability £γ₽and low maintenance σ₩↑σcost；
Independently developed G1000 N'∑αXi, G3X, G660 and G5 avionic$★s simulation systems, fully covering t≈↔∑he functions of aviation school train≠$πing subjects;
The navigation database is accur★↑<ate and does not need tλ★δ&o be calibrated one by one.
Self-developed IOS System, and ↕≠™♥the software interface is user-friendΩ•ly and customizable (advanced computer 'σ∞skills are not required).
Equipped with flight training recordin¶♠↕ g, playback, and evaluation♦ ↔ functions, helping trainees i©Ωmprove training effectiv ₩eness more efficiently.
U-WING adopts the VSV visual δ♣¥↕system that is most suitable for gen↔•±eral aviation aircraft. By combining ™→✘high-precision satellite dat≈§a with large-scale automatic $¥★δ3D modeling technology, itα✔∏§ meets the customized requirements o₩ •γf high-precision urban visual simulatα±≥≈ion, especially the p≤βrecise modeling of landmark buiδ♠★↕ldings. It is more in line with t→₩"he characteristics of visual fl'Ωλight at low altitudes for gener"σal aviation aircraft. It has won tαα₽he first prize of National Science a>₩σnd Technology Progress Aw ←§ard.
