How to simulate a fixed-wing UAV and obtain its longitudinal and lateral linear systems (LTI)
An implementation which simulates the non-linear flight dynamics of a fixed-wing unmanned areal glider with Simulink and visualizes the UAV's behavior using FlightGear.
Includes tools to calculate aerodynamic coefficients using the Tornado vortex lattice method implementation and provides a script to extract longitudinal and lateral linear systems for the trimmed gliding state.
Zitieren als
Jonas Ruesch (2024). How to simulate a fixed-wing UAV and obtain its longitudinal and lateral linear systems (LTI) (https://github.com/jrgenerative/fixed-wing-sim), GitHub. Abgerufen .
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- Aerospace > Aerospace Blockset > Guidance, Navigation, and Control (GNC) >
- Engineering > Aerospace Engineering > Flight Dynamics >
- Engineering > Aerospace Engineering > UAV >
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Erstellen Sie Skripte mit Code, Ausgabe und formatiertem Text in einem einzigen ausführbaren Dokument.
ExperimentalCarrierSimulink/code
ExperimentalCarrierSimulink/code/TornadoDebugging
ExperimentalCarrierSimulink/code/unused
ExperimentalCarrierSimulink/utilities
ExperimentalCarrierSimulink/models
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1.21.0.0 | Thumbnail added. |
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1.2.0.0 | Updated description. |
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1.1.0.0 | Description updated. |
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1.0.0.0 |
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