// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-

// THIS IS A SAMPLE CONFIGURATION FILE FOR DOING HARDWARE IN THE LOOP TESTING USING THE MAVLINK HIL INTERFACE
// IF YOU WANTED TO USE THIS YOU WOULD COPY THE CONTENTS INTO YOUR APM_Config.h FILE!


// Enable Autopilot Flight Mode
#define FLIGHT_MODE_CHANNEL	8
#define FLIGHT_MODE_1		AUTO
#define FLIGHT_MODE_2		RTL
#define FLIGHT_MODE_3 		FLY_BY_WIRE_A
#define FLIGHT_MODE_4       FLY_BY_WIRE_B
#define FLIGHT_MODE_5       STABILIZE
#define FLIGHT_MODE_6       MANUAL

// Hardware in the loop  protocol
#define HIL_PROTOCOL        HIL_PROTOCOL_MAVLINK

// HIL_MODE SELECTION
//
// Mavlink supports
// 1. HIL_MODE_ATTITUDE : simulated position, airspeed, and attitude
// 2. HIL_MODE_SENSORS: full sensor simulation
#define HIL_MODE            HIL_MODE_ATTITUDE

// HIL_PORT SELCTION
//
// PORT 0
// Port 0 is the port usually used for HIL.  You attatch your HIL computer 
// to APM using a USB cable.  You can run telemetry on Port 3
//
// PORT 1 
// Available for special situations.  This uses the port that would have 
// been used for the gps
// as the hardware in the loop port. You will have to solder 
// headers onto the gps port connection on the apm
// and connect via an ftdi cable.
// The buad rate is controlled by SERIAL1_BAUD in this mode.
//
// PORT 3
// If you don't require telemetry communication with a gcs while running
// hardware in the loop you may use the telemetry port as the hardware in
// the loop port.  Alternatively, use a telemetry/HIL shim like FGShim
// https://ardupilot-mega.googlecode.com/svn/Tools/trunk/FlightGear
//
// The buad rate is controlled by SERIAL3_BAUD in this mode.

#define HIL_PORT            0

// You can set your gps protocol here for your actual
// hardware and leave it without affecting the hardware
// in the loop simulation
#define GPS_PROTOCOL 		GPS_PROTOCOL_MTK

// Ground control station comms
#if HIL_PORT != 3
# define GCS_PROTOCOL        GCS_PROTOCOL_MAVLINK
# define GCS_PORT            3
#endif

// Sensors
// All sensors are supported in all modes.
// The magnetometer is not used in 
// HIL_MODE_ATTITUDE but you may leave it
// enabled if you wish.
#define AIRSPEED_SENSOR     ENABLED
#define MAGNETOMETER        ENABLED
#define AIRSPEED_CRUISE     25
#define THROTTLE_FAILSAFE   ENABLED