parameters: (self, nav_roll, nav_pitch, nav_bearing, target_bearing, wp_dist, alt_error, aspd_error, xtrack_error)
return_statement: return self.send(self.nav_controller_output_encode(nav_roll, nav_pitch, nav_bearing, target_bearing, wp_dist, alt_error, aspd_error, xtrack_error))
docstring: Outputs of the APM navigation controller. The primary use of this
                  message is to check the response and signs of the
                  controller before actual flight and to assist with
                  tuning controller parameters.
  
                  nav_roll                  : Current desired roll in degrees (float)
                  nav_pitch                 : Current desired pitch in degrees (float)
                  nav_bearing               : Current desired heading in degrees (int16_t)
                  target_bearing            : Bearing to current MISSION/target in degrees (int16_t)
                  wp_dist                   : Distance to active MISSION in meters (uint16_t)
                  alt_error                 : Current altitude error in meters (float)
                  aspd_error                : Current airspeed error in meters/second (float)
                  xtrack_error              : Current crosstrack error on x-y plane in meters (float)
docstring_summary: Outputs of the APM navigation controller. The primary use of this
                  message is to check the response and signs of the
                  controller before actual flight and to assist with
                  tuning controller parameters.
docstring_tokens: Outputs of the APM navigation controller . The primary use of this message is to check the response and signs of the controller before actual flight and to assist with tuning controller parameters .
function: def nav_controller_output_send(self, nav_roll, nav_pitch, nav_bearing, target_bearing, wp_dist, alt_error, aspd_error, xtrack_error):
                  '''
                  Outputs of the APM navigation controller. The primary use of this
                  message is to check the response and signs of the
                  controller before actual flight and to assist with
                  tuning controller parameters.
  
                  nav_roll                  : Current desired roll in degrees (float)
                  nav_pitch                 : Current desired pitch in degrees (float)
                  nav_bearing               : Current desired heading in degrees (int16_t)
                  target_bearing            : Bearing to current MISSION/target in degrees (int16_t)
                  wp_dist                   : Distance to active MISSION in meters (uint16_t)
                  alt_error                 : Current altitude error in meters (float)
                  aspd_error                : Current airspeed error in meters/second (float)
                  xtrack_error              : Current crosstrack error on x-y plane in meters (float)
  
                  '''
                  return self.send(self.nav_controller_output_encode(nav_roll, nav_pitch, nav_bearing, target_bearing, wp_dist, alt_error, aspd_error, xtrack_error))
function_tokens: def nav_controller_output_send ( self , nav_roll , nav_pitch , nav_bearing , target_bearing , wp_dist , alt_error , aspd_error , xtrack_error ) : return self . send ( self . nav_controller_output_encode ( nav_roll , nav_pitch , nav_bearing , target_bearing , wp_dist , alt_error , aspd_error , xtrack_error ) )