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MI8MI17 COMPLEX FLIGHT SIMULATOR

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Title: MI8MI17 COMPLEX FLIGHT SIMULATOR

1
MI-8/MI-17 COMPLEX FLIGHT SIMULATOR
2
Mi-8/Mi-17 Helicopter Complex Flight Simulator

CFS is intended for training, maintenance and
perfecting of flight crew skill level pursuant to
the affirmed curriculums and training programs
with issue of the appropriate certificates.
The Simulator enables practicing of flight crew
operation under normal (standard), complicated
and emergency flight conditions
in real time at all flight stages in conformity
with "Flight Crew Operating Manual (FCOM) within
the whole flight limitation range.

3
Actuality

Mi-8/Mi-17 is the most popular helicopter in the
world
Restricted flight hours (air transport service
reduction)
Aircraft engineering becoming more complicated
and upgraded
Increase of number of flight accidents owing to
the human factor (including non-optimum
interaction)
Flight hour cost increase
Capability of transfer of flight training onto
a simulator
Capability of technical implementation at a
modern level
Confirmation of crew minimums
Trainings after and during intervals in flights
... absence of any proposal for a modern
simulator while there is a demand for it

4
The given simulator enables to practice all tasks
in accordance with "Airworthiness Directives",
State Servive of Civil Aviation of Russian
Federation (SSCA RF), JAA,FAA

Solution of navigational tasks
Initial pilot training
Training IFR flights in day and night, visual and
bad weather conditions
Visual orientation
Practicing of skills in the operation of the
helicopter onboard systems
Practicing of flight crew interaction and
operational technique
Practicing of operation in case of equipment,
system, instrument failure
Practicing of operation under complicated and
emergency conditions
Ergonomics research of installed systems,
including rearrangement due to the change of
number of flight crew
Research of the human factor influence on
accuracy and efficiency of executed procedures

5
Training in accordance with LOFT, CRM programs

Organization of CRM seminars
Preflight briefing
Automated system of preparation of LOFT scenarios
Implementation of the constituted scenario
Flight debriefing on optimization of flight crew
interaction

6
Mi-8/Mi-17 CFS enables to practice

Preflight preparation, including navigational
aspects
Actuation and check of onboard systems, input and
check of the initial aeronautical information
Start up and test of engines and APU pursuant to
FCOM
Taxying along runway (dry and wet concrete) and
taxiways on the helicopter and making decision
for take off in the selected direction
Take-off, climb with the visual plotting of
terrain and horizon in day time and night
conditions
Enroute flight, descending, landing approach and
go-around procedure with the use of instruments
and systems in all range of operational
altitudes and speeds
Enroute flight with the use of radio navigational
aids
Emergency descent
Circling flight, landing approach, landing and
go-around and running landing
Run with application of available braking aids
Two-way radiocommunication with ground and
intercommunication by ICS
Flight crew operation in emergency and
complicated flight situations bound with failures
of airborne equipment, systems and devices,
dangerous exposures, covered by FCOM
Visual landing approach
Autorotation landing
Landing in mountains

7
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9
Mathematical Model

The most perfect and developed Mi-8/Mi-17 model
today
Model of center-of-mass motion kinematics
Model of flight dynamics (distribution of
aerodynamic forces and moments arising in flight
at all stages, starting from taxying and up to
touchdown during landing, stability and
controllability characteristics, critical flight
modes etc.)
Model of systems and equipment operation
Model of power plant (main engines and auxiliary
power unit)
World model, i.e. environmental conditions
influencing flight parameters (temperature,
atmospheric pressure, wind parameters etc.)
Model of AHRS (attitude and heading reference
system).

10
Acceleration Effect Imitator

Constant non-directional "background" motion of
the cockpit during all flight
Angular and linear accelerations and shifts in 6
degrees of freedom at break-out, braking and
moving on the ground
Angular and linear accelerations and shifts in 6
degrees of freedom, characteristic for flight
phases
Jerkiness when moving along runway
Jerkiness effects at critical angles of attack
Buffet effects in overspeed situation.

???
Electrical Dynamic Stand
11
Instructor Work Station

WORK MODES
Monitoring
Controlling
Scenario constituting and editing
Exercise analysis
Visual channel
Active situation display
Radio communication
Video monitoring

All information on flight crew operation and
flight parameters during exercise is recorded
for the consequent debriefing.
12
Acoustic Effects Imitation System

AEIS imitates a general acoustic field
in the Simulator cockpit synthesizing
all spectrum of noise arising during flight
Engines
Auxiliary power unit
Landing gear interaction with runway
Noise of landing gear destruction during
landing
Airflow interaction with the helicopter surface
Noise of precipitations
Noise, arising by instrumentation and equipment
operation

13
Visual System

Uninterrupted collimating image
Resolution 1024?768
Colours up to 16 mln.
Field of view up to 360 degrees. (depending
upon number of channels)
Scene update rate
from 25 Hz and higher
Illumination smooth and realistic transfer from
daytime and night to dusk
Visibility from clear to foggy 0 20 000 ?.

14
Visual Scene Content, Region and Size

Content
Sky
Sea
Terrain features
Lights
Smoke
Aerodrome facilities
Runway, taxiway, buildings
Navigation aids
Cultural objects
Local visibility areas change
Winter/summer
Region
Any
Size of the scenes is unlimited.
Standard supply kit includes standard scene 600
x600 km.

15
Automatic Landscape Generation

Generation mean time 20 min.
Generation from any vector formats of electronic
charts

16
Illustration of visual scenes
17
Hardware and Architecture

HARDWARE
Mechanical units of the helicopter management
system
Sensors of controls
Real controls loading system
Digital-analog converter, analog-digital
converter
Electrical circuits
PCBs of instrument panels
PC on the basis of Intel Pentium III
PC Evans Sutherland
Projectors
THE DISTRIBUTED ARCHITECTURE
CAN BUS, ETHERNET
ADVANTAGE
Smaller response time
Reliability and weight
Expanded simulation capabilities
Simple mounting and service

CAN BUS
18
Mi-8/Mi-17 CFS Advantages

Adequate mathematical Mi-8/Mi-17model
Open architecture
The production product
Costeffective implementation
Certification according to new requirements of
State Service of Civil Aviation of Russian
Federation, harmonized with the JAA and FAA
requirements
Implementation of LOFT and CRM methods
Large area of visualization scenes.

19
Practicing of Skills in Operation of New Equipment
20
Procedural flight simulator Mi-8/Mi-17

Initial pilot training
Solution of navigational tasks
Training IFR flights in day and night, visual
and bad weather conditions
Visual orientation
Initial practicing of skills in the operation of
the helicopter onboard systems
Initial practicing of flight crew interaction and
operational technique
Initial practicing of operation in case of
equipment, system, instrument failure
Initial practicing of operation under complicated
and emergency conditions

21
Variants of delivery

At the request of the Customer structure of
delivery can include
Variant 1. The training centre.
- KTV Mi-8/Mi-17 (modification 1 or modification
2), established on a mobile platform
- Procedural flight simulator Mi-8/Mi-17
The note At the request of the ?ustomer
designing and capital construction of the
training centre and complex can be included in
standard item.
Variant 2. KTV Mi-8/Mi-17 (modification 1 or
modification 2), with a mobile cabin.
Variant 3. KTV Mi-8/Mi-17 (modification 1 or
modification 2), with a motionless cabin.
Variant 4. Procedural flight simulator Mi-8/Mi-17
with a display instrument board.
Modification 1 - simulators of the onboard
equipment (panels, devices).
Modification 2 - regular onboard equipment with
simulators of devices aneroids and accelerators
groups.
All variants of delivery include multichannel
system of visualization and workplace of the
instructor.