Alexander S. Ustinov, Vladimir I. Tsimbalyuk, Tatiana I. Orlova

DOI Number: N/A

Conference number: IFASD-2015-102

The purposes of this work are the demonstration of aircraft loading specificity when regular control system (CS) operates and development of offers to minimize variable loads influencing on resource characteristics. Flight data measured on the modern aircraft are analyzed. Loading of control surfaces actuators is considered. Influence of spoiler deflections on plane units loading is shown. Results of analytical researches of CS influence on variable loads repeatability are presented.

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In Categories: 2. IFASD 2015, Loads Alleviation
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