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Fig 6
- Generic Tilt-Rotor Simulation Model with Coupled Flight Dynamics, State-Variable Aeromechanics, and Aeroacoustics
DI controller as applied to a linear system.
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Reference
Generic Tilt-Rotor Simulation Model with Coupled Flight Dynamics, State-Variable Aeromechanics, and Aeroacoustics - Scientific Figure on ResearchGate. Available from: https://www.researchgate.net/figure/DI-controller-as-applied-to-a-linear-system_fig5_370774821 [accessed 19 Feb 2025]
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Fig. 6: DI controller as applied to a linear system.
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<a href="https://www.researchgate.net/figure/DI-controller-as-applied-to-a-linear-system_fig5_370774821"><img src="https://www.researchgate.net/profile/Umberto-Saetti/publication/370774821/figure/fig5/AS:11431281161234936@1684948859165/DI-controller-as-applied-to-a-linear-system.png" alt="DI controller as applied to a linear system."/></a>
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