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This example models an vertical takeoff and landing (VTOL) aircraft and explores the workflow of designing the battery pack.
- Batteries, motors, and propellers are integrated to model the aircraft
- Parallel simulations are used to identify battery energy density requirements
- Manufacturer-specific parameters characterize the battery cell model.
- Loadcases of battery current are determined from mission simulations.
- Battery pack architectures are assembled using MATLAB commands.
- Thermal requirements are determined by setting target temperature gradients.
- Cooling plate designs are explored at the module and pack level.
Open the project file Airtaxi_VTOL.prj to get started.
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