Develop the offline system model
The supplied scope includes MATLAB/Simulink models for PMSM, EESM, IM, DFIG, SynRM and SRM systems, with functional evaluation of both controller and motor models.
Compile for real-time operation
The service description includes compiling and building real-time machine models in dSPACE. Reported aviation experience also includes dSPACE and OPAL-RT hardware-in-the-loop work.
Include the operating profile
Motor and inverter loss mechanisms can be included when examining propulsion-system efficiency over a representative application profile.
- eVTOL flight profiles
- EV WLTC and CLTC driving cycles
- Controller and plant behavior under defined test conditions
Use HIL as part of the evidence chain
Real-time testing can exercise controller behavior before or alongside hardware experiments. Model adequacy, simulator configuration and test conditions remain part of interpreting the results; HIL alone is not a product certification.
Inside the work.
Connected expertise.
Electric Aviation
Propulsion-control software development from system models to prototype aircraft flight.
Explore →
Doubly fed induction generator system diagram · supplied document · topology illustration, not the project test unit
Doubly Fed Induction Generator
Machine identification, grid-interface modeling and real-time generator control.
Explore →
Inverter loss map · supplied document
Bring semiconductor losses into the drive model.
Extract device loss characteristics from datasheets and incorporate inverter losses into propulsion-system simulation.
Explore →Bring us your challenge.
Start with your application, constraints and the decision you need to make.