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俄罗斯空气动力研究所中心学报

ISSN 打印: 1948-2590
ISSN 在线: 1948-2604

俄罗斯空气动力研究所中心学报

DOI: 10.1615/TsAGISciJ.2014011352
pages 151-168

CALCULATION OF THE AIRCRAFT DYNAMICS DURING TAKE-OFF BY RESULTS OF ONBOARD MEASUREMENTS IN ORDER TO DETECT EMERGENCY SITUATIONS

Anatoliy Vladimirovich Bobylev
Central Aerohydrodynamic Institute (TsAGI) 1, Zhukovsky str., Zhukovsky, 140180, Moscow region, Russia
Viktor Fedorovich Bragazin
Central Aerohydrodynamic Institute (TsAGI), 1 Zhukovsky Str., Zhukovsky, 140180 Russia
Vasiliy Aleksandrovich Yaroshevsky
Central Aerohydrodynamic Institute (TsAGI) 1, Zhukovsky str., Zhukovsky, 140180, Moscow region, Russia

ABSTRACT

The possibility of calculating aircraft balance, as well as other dynamic parameters, based on the discrete algorithm resulting from the condition of the root-mean-square minimum error is considered. A simplified problem without taking into account the lateral dynamics is solved, and a quasi-static model is used to determine the loads on the nose and main landing gears. The impact air pressure, longitudinal acceleration, pitch angle, and radio-altimeter readings are the measured parameters considered.


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