| CONTROL SYSTEMS, STABILIZATION, NAVIGATION, ORIENTATION AND GUIDANCE |
| D.V. Kapulin |
DYNAMIC CHARACTERISTICS OF VOLTAGE IMPULSE STABILIZER FOR SWITCHING LARGE POWER LOAD
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| B.M. Klimashov |
SELECTION OF LOW-FLYING OR LOCATED ABOVE LAND OR SEA SURFACE TARGET BY THE MEANS OF AUTONOMOUS AIRPLANE ON-BOARD RADIO LOCATING DEVICE
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| INFORMATION-MEASURING AND CONTROL COMPUTER SYSTEMS |
| P.G Michaylov, V.P.Michaylova, I.O. Lapshin |
SENSORS FOR SPACE ROCKET AND AVIATION TECHNOLOGY
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| I.J. Zmeev, P.N. Lepeshkin, D.E. Sahnin |
THE RECURSIVE ALGORITHM OF DIFFERENTIATION
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| J.A. Agamalieva |
THE HYBRID INFORMATION MODEL OF THE DIAGNOSTICS AND FORECAST OF THE CHANGE THE TECHNICAL CONDITION AIRCRAFT GAS TURBINE ENGINES
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| METHODS OF SIMULATION OF COMPLEX |
| L.N. Nikiforova |
CONSTRUCTING OPTIMAL TRAJECTORY OF NAP-OF-THE-EARTH FLIGHT ON MEDIUM DISTANCES FOR HELICOPTER
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| LIFE SUPPORT SYSTEM AND INFORMATION DISPLAY FOR AIRCRAFT CREW |
| Yu.V. Popov, A.A. Martynyuk, I.A. Krasotkina |
NOISE AS SOURCE OF INFORMATION ABOUT SITUATION IN THE CREW COCKPIT
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