Cessna C172 Fixed-base Simu"≤σ→lator

Overview

Experience Subject:

  • Normal Flight Standard Operating Proce← ±×dure (SOP) 

  • VFR Circuit Base Train£☆&<ing 

  • IFR Training 

  • Complex weather flight ∑‍✘training

  • Aircraft main failures and ✔πspecial condition training 

  • Extreme Flight training cours§$e

  • Other supplementary subjects

Flight simulation system γ 

Using a fully self-develoΩ★φped professional flight ↓‍£≥simulation platform, with a comple‍"₩te aerodynamic model and engine mo∏→γ₩del. Higher iteration freque♣♣←±ncy and faster speed.

A self-developed dat≠§₹​a collection system,♦‌® with flight test data and≥↑ engineering calculation data as data π<✔sources, based on a self-d™¶eveloped data package of flight✘® test data.

The aerodynamic model includes subject↑≤± s outside the flight envelo∏♣pe (such as stall, s♣βpiral, etc.).


Visual system

U-WING adopts the VSV visΩπ>ual system that is most suitab∑∑le for general aviation aircraft. By cΩ$∞$ombining high-precision sat∑>₽÷ellite data with large-scale automat‍ ✘φic 3D modeling technology, it meets σ¥the customized requirements of α‍≥high-precision urbanφ₽ visual simulation, especially the♠≥ precise modeling of landmark γ<↓buildings. It is more in line wi₩↔th the characteristics o≠δ∏∑f visual flight at low $≥γ∞altitudes for general a→​λviation aircraft. It has woβ↑↕n the first prize of Nation εα§al Science and Technology Progress A₩↕ward.

Technical parameters
Size(mm)
1450×1902×1788

Power(KW)
1.3
Voltage(V)
220

Temperature(°C)
5-33

Humidity(%rh)
≤75

Weight(KG)
300-500