Версия для печати
Research Flight Simulators:
Mathematical Modeling:
CAD systems:
Flight Dynamics
- development of requirements for aircraft stability, controllability and control systems
- experimental investigation of aircraft dynamics using flight simulators and with test pilots
- development of new methods of partial full-scale flight simulation
- development and creation of experimental facilities
Research Flight Simulators:
- PSPK — 102 Flight simulator with a Moving Cockpit
- PSPK — 1 Flight simulator with a Moving Cockpit
- PSPK — 2 Flight simulator with a Moving Cockpit
- PSPK-3 Flight Simulator with a Moving Cockpit (four-axis)
- PS — 10 Flight simulator with a Spherical Screen
- MK — 10 Airplanes take — off and landing simulator
- Full-scale simulators FULLSIM
- Universal simulators with displayed indicators board MIDISIM
- Mini-simulators with control levers imitators MINISIM
- Outcabin situation
Mathematical Modeling:
- Experiments in wind tunnels
- Calculation methods
- Flight tests
- Adjusting mathematical aerodynamic model
- Aircraft model
Typical Structure of Aircraft Mathematical Model:
- Mass inertial characteristics
- Engine model
- Radio and navigational systems models
- Motion equations
- Aerodynamic characteristics database
- Gear model
- Control system model
CAD systems:
- CAD system SEGAMBIS
- CAD system DOMCRIS
CAD Dynamics/Matlabsimulink:
- Aerodynamic Database
- Nonstability and hysteresis data
- Construction elasticity
- Aircraft configuration
- Influence of closeness to the ground
- Emergency situations and combat damages
Simulating Dynamics of Aircraft Controlled Motion:
- Mathematical
- Simulation with pilot at controls