You signed in with another tab or window. Reload to refresh your session.You signed out in another tab or window. Reload to refresh your session.You switched accounts on another tab or window. Reload to refresh your session.Dismiss alert
The controller interface was updated. The common handlers now contain the motor thrust curve parameters, gravitational acceleration and a getter for the current estimated UAV mass.
Moreover, the motor thrust curve parametrization is now independent on the number of motors on the UAV. The number of motors is a new parameter within the "motor params" config file. Therefore, the parameters for the same propulsion type can be shared between different UAV types. To update the config file to the new parametrization, do the following:
The old format:
hover_thrust:
a: 0.175b: -0.148
hover_thrust -> motor_params
add n_motors
multiply the old a by sqrt(n_motors)
motor_params:
n_motors: 8a: 0.4949b: -0.148
The text was updated successfully, but these errors were encountered:
The controller interface was updated. The common handlers now contain the motor thrust curve parameters, gravitational acceleration and a getter for the current estimated UAV mass.
Moreover, the motor thrust curve parametrization is now independent on the number of motors on the UAV. The number of motors is a new parameter within the "motor params" config file. Therefore, the parameters for the same propulsion type can be shared between different UAV types. To update the config file to the new parametrization, do the following:
The old format:
hover_thrust
->motor_params
n_motors
a
bysqrt(n_motors)
The text was updated successfully, but these errors were encountered: