-
Notifications
You must be signed in to change notification settings - Fork 13
New issue
Have a question about this project? Sign up for a free GitHub account to open an issue and contact its maintainers and the community.
By clicking “Sign up for GitHub”, you agree to our terms of service and privacy statement. We’ll occasionally send you account related emails.
Already on GitHub? Sign in to your account
Adding Fixed-Wing Model #115
Conversation
505eb29
to
374220f
Compare
Adding a standard wing model that corresponds to the PX4 standard plane airframe. It has ailerons but no flaps and estimated all present forces but not yet the moments.
The old fuselage drag model had an dependence on the angle of attack in x-direction. This seems very overkill given that even a single fuselage drag coefficient is hard to observe separatly from the dominant rotor drag force.
This commit adds the standard plane model and adapts the generation of the stadard vtol model to be based on this new model.
Added model configs, but still errors as below
|
This is because the data frame is filtered by the minimum PWM threshold 1500, but none of it exists:
Fixed with a hack: by moving the default index to the third actuator (which the fixedwing has a motor). |
f3ec493
to
30356df
Compare
The default index for filtering out invalid data had to be switched to the third actuator Shift index for plotting F
45263cd
to
a2c9f37
Compare
Since I think all the structure to run is now in place, I am merging this so that I can work on linking the model with simulation. I guess we can fix all the issues there 😄 Thanks @manumerous ! |
Problem Description
Since there were no fixedwing model in this pipeline, this PR adds a fixedwing model in order to test the estimation of aerodynamic parameters