Cessna C172S Level 5 FTD

Overview
  • 1:1 simulated cockpit

  • Semi-closed instructor operation εΩstation (2 touch-scre↕‍γen) 

  • GARMIN Perspect↓₹ive+ (PFD &a∞₽£mp; MFD)

  • GFC700 Auto Pilot System

  • Closed-loop control loading s←♠ystem

  • Electrical pitch and roll trim

  • VSV HD 3 Channel Visual System


Flight simulation syste"$m

Using a fully self-developed prφ​ε§ofessional flight simul♦™ation platform, with a φ₽complete aerodynamic model anδ×≥​d engine model. Highe δ¶★r iteration frequency an✘∏∑πd faster speed.

A self-developed data ₩‌collection system, with fli‍ ✘δght test data and engineer∑©ing calculation data as data★♠ sources, based on a self-develope><✔d data package of flight test data.®Ω

The aerodynamic model includes subject±₩∑s outside the flight enveloα¥pe (such as stall, sp₩↕ iral, etc.).

The simulation level is ✔α←σhigher than the requirements of&nbs♥↑✔p; FTD5, which can demons© →trate individual charact★¥eristics specific to specific airc¥λ↔raft models.

Avionics system

The  avionics si‌∞mulation system is s♥σelf-developed by U-Wing, and it is st₹≤>¶able and reliable unδα®der Linux operating system.;

The simulation hardware is the s÷₩ame as the real aircra★¥δ→ft, with high reliabi₹±lity and low maintenance cost;

Independently developed©φ&↕ G1000 NXi, G3X, G660 andβφ G5 avionics simulation systems, f ↕♦∏ully covering the fun∞ε♠ctions of aviation school training ₽ £↑subjects;

The navigation database i£™→≠s accurate and does not need to be ca↔Ω©♦librated one by one.

Instructor control system ∞₩☆α

Self-developed IOS System, and the &×software interface is user-friendly δ×εand customizable (advanced comput↑> er skills are not re≠← αquired).

Equipped with flight tra ≠∑±ining recording, play¥&back, and evaluation funct♥‌ ions, helping trainees improve trai$♣γ₩ning effectiveness more efficiently.

Visual system

U-WING adopts the VSV vi♠§σsual system that is most suitable foλ↕r general aviation aircraft. By combini∞§ε♣ng high-precision satell↓×ite data with large-scale au‍♥"★tomatic 3D modeling technology, it m∑‍eets the customized requi± ☆♦rements of high-prec‍​¶ision urban visual simula↑↔tion, especially the p©&♠'recise modeling of landmark buildi♣∑ngs. It is more in line wi÷✔ <th the characteristics of visual f≤₩<light at low altitudes for g λeneral aviation aircraft. It has won t♠₩‍he first prize of Natio↑$☆nal Science and Techno©↑ ≥logy Progress Award.