TYPICAL MOTIONS OF A FINNED BODY IN RESISTANT MEDIUM
V. Samsonov, Yu. Okunev, O. Privalova
Tsiolkovsky MATI, Institute of Mechanics of Lomonosov MSU

DESIGN EXPERTISE AND EVOLUTION OF INFORMATION DISPLAY SYSTEMSAND TRAINING SYSTEMS FOR MANNED SPACECRAFT
V. Bezrodnov, Y. Kasatikov, A. Suvorov
JSC “Institute of Aircraft Equipment”

SIMULATION OF AIRCRAFT UPSET RECOVERY ON RESEARCH AND TRAINING FLIGHT SIMULATORS
Bushgens A.G., Grigoriev M.A., Khrabrov A.N., Yashin Y.P., Zaichik L.E.
TsAGI

Is not presented in English

MODELING AND ESTIMATION OF THE PHOBOS-GRUNT PARAMETERS OF MOTION AND RE-ENTRY
Golubtsova N.A., Kolyuka Yu.F., Afanaseva T.I., Gridchina T.A.
Mission Control Center, Central Research Institute of Machine Building,

IMPROVED METHODS FOR THE METEOR OBSERVATIONS INTERPRETATION AND THEIR APPLICATIONS
Gritsevich M.I. 1, 2, Kuznetsova D.V. 1, 2, Stulov V.P. 1, 2, Turchak L.I.3
1 Institute of Mechanics of the Lomonosov Moscow State University; 2 Faculty of Mechanics and Mathematics of the Lomonosov Moscow State University; 3 Dorodnitsyn Computing Center

MODELLING OF PARAMETERS OF THE ATMOSPHERE IN AREAS OF START OF LAUNCH VEHICLES
Denisova I.P., Kalnin P.P., Muravey L.A., Piliya V.K., Pokrovskiy A.N.
MATI - the Russian state technological university of a name of K.E.Tsiolkovsky

 METHODOLOGY OF A.M.LYAPUNOV STABILITY THEORY IN PROBLEM OF THE MOTIONS SEPARATION FOR SGS
L.K.Kuzmina
KNRTU-KAI

THEORETICAL STUDY AND MODELLING OF THE SAFE TURN MANOEUVRES OF AGRICULTURAL AIRCRAFT
Bosko Rasuo
University of Belgrade, Belgrade, Serbia,

THE METHODIC OF CORRECTION OF THE MATHEMATICAL MODEL OF THE CARRIER-BASED AIRCRAFT AT REGIMES OF TAKEOFF AND LANDING
Korsun O.N., Nikolaev S.V.
MAI

POWER ENGINE THRUST AND AERODYNAMIC DRAG EVALUATION USING FLIGHT TEST
Poplawski B.K., Korsun  O.N., Leonov V.A.
Gromov Flight Research Institute; MAI

OPTIMAL CONTROL SYNTHESIS FOR DYNAMIC SYSTEMS, ADAPTIVE TO MEASURED DISTURBANCES
Korsun O.N1., Kharkov V.P.2
1MAI;  2VVA

MATHEMATICAL MODELS OF AIRBORNE SPEED AND ANGLE OF ATTACK MEASUREMENT ERROR FOR AIRCRAFT LANDING MODE
Pushkov S.G., Gorshkov O.Y.,Gromov Flight Research Institute; Korsun O.N., MAI

THE IDENTIFICATION OF ATTITUDE CONTROL SYSTEM OF MULTIMODULAR ORBITAL SPACECRAFT UNDER MEASUREMENTS OF ANGULAR MOTION USING THE METHOD OF TRAINED MODELS
M.V. Levskii
Research Institute of Space Systems (Khrunichev State scientific & production Space Center)

AIR VEHICLE NAVIGATION  ON EARTH GEOPHYSICAL FIELD
Nikulin S.A,  Scientific Designed Center «Region»; Stupnev V.U. Tactical missile weapon Corporation

RESEARCH SEMINATURAL SIMULATOR FOR PILOTING TASKS AND FLIGHT DATA PROCESSING ANALYSIS
Korsun O.N., Burlak E.A., Nabatchikov A.M.
GosNIIAS

A PROTOTYPE OF ROBOTICS SMALL-SCALE HELICOPTER
Pshihopov V. Kh., Sergeev N. E., Kulchenko A. E.
Taganrog Institute of Technology of Southern Federal University, The Department of Electrical

OPTIMIZATION OF THE EQUATIONS OF THE MOTION ROTATING BODIES
Samsonov V.A. Belyakov D.V.
«MATI - the Russian state technological university of K.E. Tsiolkovsky»

ABOUT EVALUATION OF THE CONTROL MODES’ EFFICIENCY OF SPACECRAFTS
RE-ENTERING THE MARS ATMOSPHERE
Sokolov N.L., Kozlov V.G.
Federal unitary state enterprise «Central scientific research institute of machine building»

 Is not presented in English

ASTER Program Package for the Through Trajectory Optimization based on the Pontryagin maximum principle
Filatyev A.S., Yanova O.V., Golikov A.A.
Central Aerohydrodynamic Institute named after prof. N.E. Zhukovsky (TsAGI)

COMPLEX STRENGTH ANALYSIS OF CARRIER ROCKET BODY ON THE BASIS OF MULTILEVEL PARAMETRICAL FEM MODELS
Dubovikov E.A., Kondakov I.O., Shanygin A.N.
Central Aerohydrodynamic Institute named after prof. N.E. Zhukovsky

PROBLEMS RELATING TO CALCULATION OF DROP ZONES FOR LV SEPARATED PARTS
Eliseykin S.A., Podrezov V.A., Poluarshinov A.M. 
FGUP TsENKI

OPERATED RELATIVE MOVEMENTS ORBITAL ROPING SYSTEMS ON THE BASIS OF THE QUALITATIVE THEORY OF DYNAMIC SYSTEMS
Ivanov V. A., Ruchinsky V.S.,
«MATI - the Russian state technological university of K.E.Tsiolkovsky».

INCREASE IN RANGE OF FLIGHT OF THE FLYING MACHINE BY MEANS OF  ROPING SYSTEMS IN THE MODE ROTATIONS ROUND THE CENTER OF WEIGHTS
Ivanov V. ARuchinsky V.S.
«MATI - the Russian state technological university of K.E. Tsiolkovsky»

MODELING OF THE ATMOSPHERE PARAMETERS AT START-UP LAUNCH VEHICLES
Eliseykin S. A., Ivanov P. V., Shirshov N. V.
Federal State Unitary Enterprise «Center for Ground-based Space Infrastructure Facilities Operation (TsENKI)»

LONG-TERM MAINTAINANCE OF REQUIRED POINTING OF SPINNING SPACECRAFT WITH CONTROL JETS
Suprunenko S.N.
Central Aerohydrodynamic  Institute named after Prof. N.E.Zhukovsky (TsAGI)

RE-ENTRY GUIDANCE OF SPACECRAFT WITH SMALL AERODYNAMIC LIFT-TO-DRAG RATIO
Anoshin Yu.M., Bobilev A.V., Yaroshevsky V.A.
Central Aerohydrodynamic  Institute named after Prof. N.E. Zhukovsky (TsAGI)