TsAGI Science Journal
Publicado 6 números por año
ISSN Imprimir: 1948-2590
ISSN En Línea: 1948-2604
CALCULATION OF THE AIRCRAFT DYNAMICS DURING TAKE-OFF BY RESULTS OF ONBOARD MEASUREMENTS IN ORDER TO DETECT EMERGENCY SITUATIONS
Volumen 45,
Edición 2, 2014,
pp. 151-168
DOI: 10.1615/TsAGISciJ.2014011352
SINOPSIS
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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