RLBench/envs/_quadrocopter/quadrotor_dynamics.py
def dynamics_derivative(self, pitch, roll, z_vel, yaw_vel):
        """Return the state derivatives for the current state and input."""
        rates = self._inputs_to_desired_rates(pitch, roll, z_vel, yaw_vel)

        forces = self._determine_forces(*rates)

        return self._forces_to_derivatives(forces)
Return the state derivatives for the current state and input.
Return the state derivatives for the current state and input.
Return the state derivatives for the current state and input .
def dynamics_derivative(self, pitch, roll, z_vel, yaw_vel):
        rates = self._inputs_to_desired_rates(pitch, roll, z_vel, yaw_vel)
        forces = self._determine_forces(*rates)
        return self._forces_to_derivatives(forces)
def dynamics_derivative ( self , pitch , roll , z_vel , yaw_vel ) : rates = self . _inputs_to_desired_rates ( pitch , roll , z_vel , yaw_vel ) forces = self . _determine_forces ( * rates ) return self . _forces_to_derivatives ( forces )
Return the state derivatives for the current state and input.
Return the state derivatives for the current state and input .
"""Return the state derivatives for the current state and input."""
self
pitch
roll
z_vel
yaw_vel