Investigation and Application of the Helicopter Typical Flight States Identification

Zhen Hua Wan

doi:10.4028/www.scientific.net/AMM.86.556

Paper Titles

Application of Contact Analysis in Strength Analysis of Helicopter Transmission System
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Adaptive Impulse Controller Design of Harmonic Drives System with Friction
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Research on Geometry Relationship of Pin-Rack Gearing
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Coupled Motion Control and Adjustment in Automatic Programming System of CNC Hobbing Machines
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Investigation and Application of the Helicopter Typical Flight States Identification
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The Optimization Design for Rack Tooth Profile Curve of Straight Push-Rod Linear Reducer
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Mechanisms of Synchronous Belt Tooth Failure due to Fatigue Shear Fracture
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Precision Involute Gearboxes
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Study on Face Gear's Bending Stress Based on Test and Finite Element Analysis Method
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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 86Investigation and Application of the Helicopter...

Investigation and Application of the Helicopter Typical Flight States Identification

Abstract:

Typical flight states are the most important checking items during the helicopter flight-test. This article intends to illustrate the typical flight states identification method via introducing the basic theory and characteristics of helicopter control, and then apply this method to load analysis and compilation of loads spectrum.