| DESIGN AND TECHNOLOGY OF PRODUCTION OF COMPLEX OF AIRCRAFT |
| В. V. Viktorov, V.D. Eliseev |
Peculiarities of the aircraft control system drive dynamics in the case of stretched airframes and the uses of linear accelerometers signals
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| S.A. Antsiferov, L.I. Mogilevich |
Disturbing moment in floating pendulum accelerometer at asymmetric leakage of liquid into butt ends
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| A.V. Molchanov, V.M. Suminov, M.V. Chirkin |
Formation of the dominating error of the laser gyroscope
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| A. V. Molchanov, V.M. Suminov, M, V. Cltirkin |
Modelling the processes of degrading in the discharge of helium-neon ring laser
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| INFORMATION-MEASURING AND CONTROL COMPUTER SYSTEMS |
| A.V. Vorobjev |
Application of the automated simulation methods of control systems and air complexes designing
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| V.S. Ermakov, A.P. Kolevatov |
Hardware-software complex for debugging and testing algorithmic and software support of navigating systems
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| A.P. Kolevatov |
Object-oriented designing of algorithmic and software support of navigating systems
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| A.M. Selivanov, V. V. Vatolin, A.I. Teterevyatnikov, S.B. Burak |
Research into linearized dynamic simulator of perspective adaptive aviation catapult
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| MONITORING, DIAGNOSIS AND TESTING OF AIRCRAFT |
| A.V. Eliseev |
Method of compensating of singular errors
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| LIFE SUPPORT SYSTEM AND INFORMATION DISPLAY FOR AIRCRAFT CREW |
| N.S. Melnikov, T. V. Shevel |
Synthesis of the functionally reliable control system of the aircraft unpowered landing with rational distribution of functions between automatic control system and crew
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