International Institute for Advanced Aerospace Technologies – IIAAT
Educational Programs • Postgraduate and Research • Advanced Projects Management
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Purpose
Background
Educational programs
Short term lecturing programs
Engineering training in English medium
Themes for students training in IIAAT in 2020
PhD Degree in Mathematics
Research
Staff
Leadership
C.V. of Prof. A.Nebylov
Some scientific achievements
Some research & development projects
Ekranoplane «Spasatel» presentation
TEMPUS Project
«Aerospace Sensors» book
«Aerospace Navigation Systems» book
Nano-Technology
Individual Themes for Master Students Training in 2020 in Aerospace Instrumentation and Control
Modern approach to aerospace vehicle navigation and motion control systems optimization
Space Vehicle trajectory control
Methods of active stabilization of space vehicle
Methods of passive stabilization of space vehicle
Bending modes control
Algorithms of flexible vehicle stabilization
Sloshing modeling and simulation for control laws design
Experimental testing of vehicle flexibility
Optimization of onboard sensors installation points
Selection and investigation of gyros for aerospace vehicles
Selection and investigation of accelerometers for aerospace vehicles
Inertial systems design for aerospace vehicles
Sensors Integration for inertial navigation system
Self Alignment of inertial system
Gimbals inertial navigation and attitude control
Strapdown inertial navigation and attitude control
Theory and design of micromechanical gyros and accelerometers
Inertial sensors on surface acoustic waves (SAW)
Sensors of aerial medium for aerospace vehicles
Control laws for aerospace vehicles docking
Principles of altitude measuring for space vehicles landing
Control laws for reentry vehicles
Satellite attitude control
Star sensors application for space probes attitude and motion control
Modern control theory in application to aerospace vehicles investigation
Control accuracy ensuring methods for aerospace control systems
Control laws synthesis in the frequency and time domains
Digital control systems design for aerospace application
Computers and digital hardware selection for aerospace application
Structural redundancy application for space vehicle control systems
Advanced conceptions of space transportation systems design
Comparison of VTVL and HTHL space vehicles advantages
Peculiarities of aerospace plane horizontal launch with ekranoplane assist
Peculiarities of aerospace plane horizontal landing
Relative motion control at aerospace plane horizontal landing on ekranoplane
WIG-craft (ekranoplanes) advanced design and control principles
SNS (GPS and Glonass) application for space vehicle motion control
Radio systems for short-range navigation
Landing Radio systems
Satellite navigation systems design principles
Terrestrial images processing algorithms
Image compression methods and algorithms
Homing systems
Infra-red sensors and systems
Map matching navigation systems
Themes for students short-term training in IIAAT in 2020-2021
I. Investigation of flying vehicles, including Wing-In-Ground effect craft
Problems of multistage aerospace vehicles design.
Analysis of peculiarities and comparative effectiveness of flying vehicles with vertical take-off and landing (helicopters, planes with turned vector of thrust, hovercraft, WIG-craft with blowing under the wing), comparison at fuel saving and other criteria.
Analysis of the areas of the most effectual application of WIG-craft in compare with other kinds of air transportation.
Effectiveness analysis of heavy WIG-craft assist at aerospace plane horizontal launch and landing.
Investigation of sea waves statistical characteristics and their influence on the fast sea transport (mainly WIG-craft) motion.
Key problems of homing missiles perfecting.
General principles of missiles guidance.
Key problems of aircraft perfecting.
Key problems of helicopters perfecting.
Key problems of launch vehicles perfecting.
II. Navigation and motion control systems of aerospace vehicles
Investigation of peculiarities of GPS and Glonass airborne application.
Comparative analysis of design principles and accuracy characteristics of the airborne sensors of flight altitude.
Comparative analysis of design principles and accuracy characteristics of the airborne inertial systems.
Investigation of methods of low altitude flight parameters measuring on the basis of radioaltimeters and inertial sensors integration.
Stabilization and control laws synthesis for flexible aerospace constructions.
Methods of maximum error investigation in motion control systems of flying vehicles.
Methods of automatic control systems with required accuracy indexes synthesis.
Digital system for helicopter longitudinal motion stabilization: synthesis, analysis, motion simulation.
Digital system for WIG-craft motion stabilization: synthesis, analysis, motion simulation.
Integrated digital navigation system of aircraft: algorithms of VOR/DME, GPS, course system, system of air signals measurements processing.
Problems of a micromechanical inertial sensors design: stabilization of primary oscillations amplitude of a micromechanical gyroscope.
Problems of a micromechanical inertial sensors design: design of the measuring channel of a micromechanical gyroscope.
Problems of a micromechanical inertial sensors design: minimization of output noise in micromechanical gyroscope.
Embedded Kalman filter in a micromechanical gyroscope.
III. Information and data processing
Advanced methodology of Kalman filters application in flying vehicles navigation and motion control systems.
Modern methods of parameters identification in airborne automatic control systems.
Methods of dynamic systems accuracy ensuring at incomplete a priori information about excitations.
Images compression methods for remote control systems.
Specific methods of digital control systems synthesis for flying vehicles with low cost computers.
Investigation of technology and animation movie development of aerospace plane landing at the moving WIG-craft.
Internet-conception development for students’ remote access to the software package for flexible aerospace vehicles simulation.
Address: IIAAT, SUAI, 67, Bolshaya Morskaya, Saint-Petersburg, 190000, RUSSIA
Phone: +7 (812) 494-70-16; Fax: +7 (812) 494-70-18; E-mail:
iiaat@aanet.ru