JUSTIFICATION OF THRUST VECTOR DEFLECTION OF TWIN-ENGINE UNMANNED AERIAL VEHICLE POWER PLANTS.
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- Aviation (1648-7788), 2011, v. 15, n. 1, p. 25, doi. 10.3846/16487788.2011.566319
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Works matching IS 16487788 AND DT 2011 AND VI 15 AND IP 1
Results: 4
1
2
A LOGISTIC APPROACH FOR DESCRIPTION OF DECISION-MAKING PROCESS.
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- Aviation (1648-7788), 2011, v. 15, n. 1, p. 21, doi. 10.3846/16487788.2011.566316
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- Article
3
MATHEMATICAL MODELS OF THE CALCULATION OF AIRCRAFT STRUCTURAL RELIABILITY.
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- Aviation (1648-7788), 2011, v. 15, n. 1, p. 11, doi. 10.3846/16487788.2011.566315
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- Article
4
ERROR ANALYSIS OF THE INERTIAL MEASUREMENT UNIT.
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- Aviation (1648-7788), 2011, v. 15, n. 1, p. 5, doi. 10.3846/16487788.2011.566311
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- Article