Diamond DA40/Cessna C172 Singγ→φ₹le-Seat Simulator

Overview
  • Designed specifically for&nb∞ε→♦sp; teenagers’aviation φ&≤$science program

  • Professional IOS Systδ§em, touch screen IOS '♦software. Training elements such as↓"  aircraft, environment and failure  ®>≤can be configured through the IO≠​‌‍S platform  

  • Many situational course Settings meet f&α∏lexible and diverse flight experi↕₹≤♦ence and training needs, redu$ε​↔cing the difficulty gα₩ ≠radient of beginners

  • Self-developed visual system:VSV, ♦↕↓←It can simulate various airport enviro✔ε™nment, time, vehicle information,>>♥' weather and ocean conditions • ↑and other scene

 Experience Subjectβπ ₩

  • Beginner guidance flight trainiβ✘≠♥ng

  • VFR Circuit Base Training 

  • IFR Training 

  • Complex weather flig∏≤←&ht training

  • Aircraft main failure↑<s and special

  • condition training 

  • Extreme Flight training course

  • Other supplementary subjects

Flight simulati©αon system

Using a fully self-developed professλδ"‍ional flight simulation platform, witπ≈'h a complete aerodynamic modλ≤el and engine model. Higher iteβ> ration frequency andו•≠ faster speed.

A self-developed da← ✔☆ta collection system, with flight test©♦φ data and engineering calcula§εtion data as data sources∞←↓φ, based on a self-developeα∞d data package of fliδ©≠ght test data.

The aerodynamic model includes€σ∞ subjects outside the fl ≈ight envelope (such as stal₽←εl, spiral, etc.).

The simulation level is higher tha ≠n the requirements of  FTD5,∏φ™ which can demonstrate individual ★↓πcharacteristics specific to s¥←pecific aircraft models.

Visual system

U-WING adopts the VSV visual system t$ '÷hat is most suitable for ge‌≠neral aviation aircraft. By combining ☆‍¥high-precision satellite d→σ♦ata with large-scale automatic 3D model ™♥‌ing technology, it meets the cus> ♦tomized requirements of high-precisi≤₹on urban visual simulation, especi<₩ ​ally the precise modeling of ↑λ☆landmark buildings. It is more in line ÷®↑with the characteristics of visual₩​§λ flight at low altitudeλσs for general aviation aircraft. It has©≠ won the first prize o₽★←f National Science and Technol →βogy Progress Award.

Technical parameters
Size(mm)
2270×1925×1817

Power(KW)
1
Voltage(V)
220

Temperature(°C)
5-33

Humidity(%rh)
≤75

Weight(KG)
200