Hello, thank you for publishing the model, but I encountered two issues while using it:
1: May I ask how you handle the aerodynamic data of F16? I would like to change this model to a low fidelity model, which requires low fidelity data. How should I proceed;
2: When I use the trim toolbox, it always exceeds the range of aerodynamic parameters when searching for trim points, causing the model to stop working. How should I handle this?
The trim routing doesn't incorporate inequality constraints yet, so it may generate infeasible trim points. If such a constraint would be imposed, the optimization could also result in infeasibility. This means it is physically impossible to trim the aircraft at the specified configuration.
Hello, thank you for publishing the model, but I encountered two issues while using it: 1: May I ask how you handle the aerodynamic data of F16? I would like to change this model to a low fidelity model, which requires low fidelity data. How should I proceed; 2: When I use the trim toolbox, it always exceeds the range of aerodynamic parameters when searching for trim points, causing the model to stop working. How should I handle this?