Analysis of Helicopter Slung-Load Instabilities with AFCS Feedback using Coupled Linearised Models

Analysis of Helicopter Slung-Load Instabilities with AFCS Feedback using Coupled Linearised Models
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Analysis of Helicopter Slung-Load Instabilities with AFCS Feedback using Coupled Linearised Models
Authors / Details: Rhys Lehmann, Defence Science and Technology Group; David Howe, Advanced VTOL Technologies
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Analysis of Helicopter Slung-Load Instabilities with AFCS Feedback using Coupled Linearised Models
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