| DESIGN AND TECHNOLOGY OF PRODUCTION OF COMPLEX OF AIRCRAFT |
| В.Э. Джашитов, В.М. Панкратов, В.И. Улыбин и др. |
Influencing of thermal effects on the pressure transducer for space flight vehicles
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| В.Э. Джашитов, В.М. Панкратов, В.И. Улыбин и др. |
Method "thermal shadows" of calculation and rendition of temperature fields of space engineering devices with allowance dynamics of relative movement its structural members
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| А.А. Папко |
On low-frequency force-balance accelerometer dynamic behavior formation rules
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| Н.Д. Сёмкин, А.В. Пияков, К.Е. Воронов |
The simulator of space dust plasma
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| Н.Д Сёмкин, В.Л. Балакин, К.Е. Воронов, А.В. Пияков |
The device for detection of outflow of air from the International space station
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| MONITORING, DIAGNOSIS AND TESTING OF AIRCRAFT |
| В.И. Васильев, С.С. Валеев, А.А. Шилоносов |
Design of multivariable adaptive control system of gas-turbine engine on the base of neural networks
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| Ю.С. Кабальнов, И.В. Кузнецов |
The information capacity increase of flying vehicles telecommunication systems
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| В.М. Солдаткин |
Information control system of airplane flight safety
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| В.М. Терентьев |
The stability analysis of nonlinear deviation feedback structure in vertical UAV"s maneuvering
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| Д.И. Кардаш, А.В. Кудрявцев, А.Р. Нурутдинов и др. |
The methodology of optimal architecture electronic aviation engines control systems design
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