The attitude in the aeronautical frame (right-handed, Z-down, X-front,
                Y-right).

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                roll                      : Roll angle (rad, -pi..+pi) (float)
                pitch                     : Pitch angle (rad, -pi..+pi) (float)
                yaw                       : Yaw angle (rad, -pi..+pi) (float)
                rollspeed                 : Roll angular speed (rad/s) (float)
                pitchspeed                : Pitch angular speed (rad/s) (float)
                yawspeed                  : Yaw angular speed (rad/s) (float)

def attitude_send(self, time_boot_ms, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed, force_mavlink1=False):
                '''
                The attitude in the aeronautical frame (right-handed, Z-down, X-front,
                Y-right).

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                roll                      : Roll angle (rad, -pi..+pi) (float)
                pitch                     : Pitch angle (rad, -pi..+pi) (float)
                yaw                       : Yaw angle (rad, -pi..+pi) (float)
                rollspeed                 : Roll angular speed (rad/s) (float)
                pitchspeed                : Pitch angular speed (rad/s) (float)
                yawspeed                  : Yaw angular speed (rad/s) (float)

                '''
                return self.send(self.attitude_encode(time_boot_ms, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed), force_mavlink1=force_mavlink1)