NDLI: Plenary session

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2012 2nd International Conference "Methods and Systems of Navigation and Motion Control" (MSNMC)

Table of contents

Plenary session

Perspectives of integrated inertial-satellite systems development of civil aviation aircraft

Nonlinear analysis and tracking control of advanced airframe aircraft

Gyro-free accelerometer-based SINS: Algorithms and structures

Session A: Methods, algorithms and means of navigation and motion control systems computer-aided design

Computer-integrated navigation complex of unmanned aerial vehicles

Photopolarimetric method of estimating the accuracy characteristics of onboard vertical meters in flight tests

Method of complex processing of navigation information for vehicle

Kalman filter stationarity analysis in the problem of INS errors estimation

Theoretical framework to costruct optimal flight safety diagnostic procedures

Simulator as a teaching system

Aircraft's trajectory in the compressed time scale prediction as the flight control on-board systems intellectualization

Visual SLAM algorithm using correlation extremal principle

Combined complementary filter For inertial navigation system

Method for predicting a failure risk of the UAV navigation systems

Minimization of the mean access time to the hierarchical memory system

Intelligent capacitance sensor with Linearization of transfer characteristic

The substantiating number of recommendations for creation a simulator for UAV operator training

Evaluation of aerodynamic coefficients of longitudinal short-time movement of aircraft

Software of aviation structures' bench tests

Modern computer-aided design systems of navigation and traffic control

Structure of a program and technical complex of the automated control system navigation and motion control

Use of Kalman filter in orientation systems

The choice of the solution filtration approaches in task of orientation

Synthesis of truncated filters in task of orientation

Session B: Methods and algorithms of adaptive, robust and optimal motion control systems synthesis

Robust optimization of the inertially stabilized platforms

Least squares criterion using to improve the TRIAD algorithm

Optimization of decision-making process of air traffic controller in extra situations at the airport

Reconfigurable flight control system design for aircraft when unexpected problem occurs during flight

Modeling temperature errors in coriolis vibratory gyroscopes

Whole angle approximations of aerodynamic coefficients

State space identification of flight dynamics models

Optoelectronical method of measuring phases difference

Application of Sheynin's plural calculations method at the initial stages of complex technical object design

MEMS technology microthrusters and nanoenergetic materials for micropropulsion systems

Nanotechnology enabled self-sustained power systems and high-power-density electronics for autonomous flight vehicles

Application of exceptional non-normalized quaternions, five-dimensional rotation vectors and their algebras in problems of inertial orientation

Non-classical conjugate vectors and polar differential equations of rotation in orientation problem

Evaluation of delays encountered in control of UAV

Analysis of system control unmanned aerial vehicle

Automatic control system of low-altitude flight UAV

Flying of the UAV by the solar energy

Ethernet based aircraft control

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