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# Note: If not both pitch_direct and throttle_direct are finite, then either altitude or height_rate must be finite

float32 altitude  			# [m] Altitude setpoint AMSL, NAN if not controlled
float32 height_rate 			# [m/s] NAN if not controlled directly, used as feedforward if altitude is finite
float32 equivalent_airspeed 		# [m/s] NAN if system default should be used
float32 pitch_direct 			# [rad] NAN if not controlled, overrides total energy controller
float32 throttle_direct 		# [0,1] NAN if not controlled, overrides total energy controller