You can not select more than 25 topics
Topics must start with a letter or number, can include dashes ('-') and can be up to 35 characters long.
695 lines
26 KiB
695 lines
26 KiB
// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- |
|
|
|
#include <AP_Common.h> |
|
#include <AP_Progmem.h> |
|
#include <AP_Param.h> |
|
#include <AP_Mount.h> |
|
|
|
// Just so that it's completely clear... |
|
#define ENABLED 1 |
|
#define DISABLED 0 |
|
|
|
#if defined( __AVR_ATmega1280__ ) |
|
# define MNT_JSTICK_SPD_OPTION DISABLED // Allow RC joystick to control the speed of the mount movements instead of the position of the mount |
|
# define MNT_RETRACT_OPTION DISABLED // Use a servo to retract the mount inside the fuselage (i.e. for landings) |
|
# define MNT_GPSPOINT_OPTION ENABLED // Point the mount to a GPS point defined via a mouse click in the Mission Planner GUI |
|
# define MNT_STABILIZE_OPTION DISABLED // stabilize camera using frame attitude information |
|
# define MNT_MOUNT2_OPTION DISABLED // second mount, can for example be used to keep an antenna pointed at the home position |
|
#else |
|
# define MNT_JSTICK_SPD_OPTION ENABLED // uses 844 bytes of memory |
|
# define MNT_RETRACT_OPTION ENABLED // uses 244 bytes of memory |
|
# define MNT_GPSPOINT_OPTION ENABLED // uses 580 bytes of memory |
|
# define MNT_STABILIZE_OPTION ENABLED // uses 2424 bytes of memory |
|
# define MNT_MOUNT2_OPTION ENABLED // uses 58 bytes of memory (must also be enabled in APM_Config.h) |
|
#endif |
|
|
|
const AP_Param::GroupInfo AP_Mount::var_info[] PROGMEM = { |
|
// @Param: MODE |
|
// @DisplayName: Mount operation mode |
|
// @Description: Camera or antenna mount operation mode |
|
// @Values: 0:retract,1:neutral,2:MavLink_targeting,3:RC_targeting,4:GPS_point |
|
// @User: Standard |
|
AP_GROUPINFO("MODE", 0, AP_Mount, _mount_mode, MAV_MOUNT_MODE_RETRACT), // see MAV_MOUNT_MODE at ardupilotmega.h |
|
|
|
#if MNT_RETRACT_OPTION == ENABLED |
|
// @Param: RETRACT_X |
|
// @DisplayName: Mount roll angle when in retracted position |
|
// @Description: Mount roll angle when in retracted position |
|
// @Units: Centi-Degrees |
|
// @Range: -18000 17999 |
|
// @Increment: 1 |
|
// @User: Standard |
|
|
|
// @Param: RETRACT_Y |
|
// @DisplayName: Mount tilt/pitch angle when in retracted position |
|
// @Description: Mount tilt/pitch angle when in retracted position |
|
// @Units: Centi-Degrees |
|
// @Range: -18000 17999 |
|
// @Increment: 1 |
|
// @User: Standard |
|
|
|
// @Param: RETRACT_Z |
|
// @DisplayName: Mount yaw/pan angle when in retracted position |
|
// @Description: Mount yaw/pan angle when in retracted position |
|
// @Units: Centi-Degrees |
|
// @Range: -18000 17999 |
|
// @Increment: 1 |
|
// @User: Standard |
|
AP_GROUPINFO("RETRACT", 1, AP_Mount, _retract_angles, 0), |
|
#endif |
|
|
|
// @Param: NEUTRAL_X |
|
// @DisplayName: Mount roll angle when in neutral position |
|
// @Description: Mount roll angle when in neutral position |
|
// @Units: Centi-Degrees |
|
// @Range: -18000 17999 |
|
// @Increment: 1 |
|
// @User: Standard |
|
|
|
// @Param: NEUTRAL_Y |
|
// @DisplayName: Mount tilt/pitch angle when in neutral position |
|
// @Description: Mount tilt/pitch angle when in neutral position |
|
// @Units: Centi-Degrees |
|
// @Range: -18000 17999 |
|
// @Increment: 1 |
|
// @User: Standard |
|
|
|
// @Param: NEUTRAL_Z |
|
// @DisplayName: Mount pan/yaw angle when in neutral position |
|
// @Description: Mount pan/yaw angle when in neutral position |
|
// @Units: Centi-Degrees |
|
// @Range: -18000 17999 |
|
// @Increment: 1 |
|
// @User: Standard |
|
AP_GROUPINFO("NEUTRAL", 2, AP_Mount, _neutral_angles, 0), |
|
|
|
// @Param: CONTROL_X |
|
// @DisplayName: Mount roll angle command from groundstation |
|
// @Description: Mount roll angle when in MavLink or RC control operation mode |
|
// @Units: Centi-Degrees |
|
// @Range: -18000 17999 |
|
// @Increment: 1 |
|
|
|
// @Param: CONTROL_Y |
|
// @DisplayName: Mount tilt/pitch angle command from groundstation |
|
// @Description: Mount tilt/pitch angle when in MavLink or RC control operation mode |
|
// @Units: Centi-Degrees |
|
// @Range: -18000 17999 |
|
// @Increment: 1 |
|
|
|
// @Param: CONTROL_Z |
|
// @DisplayName: Mount pan/yaw angle command from groundstation |
|
// @Description: Mount pan/yaw angle when in MavLink or RC control operation mode |
|
// @Units: Centi-Degrees |
|
// @Range: -18000 17999 |
|
// @Increment: 1 |
|
AP_GROUPINFO("CONTROL", 3, AP_Mount, _control_angles, 0), |
|
|
|
#if MNT_STABILIZE_OPTION == ENABLED |
|
// @Param: STAB_ROLL |
|
// @DisplayName: Stabilize mount's roll angle |
|
// @Description:enable roll stabilisation relative to Earth |
|
// @Values: 0:Disabled,1:Enabled |
|
// @User: Standard |
|
AP_GROUPINFO("STAB_ROLL", 4, AP_Mount, _stab_roll, 0), |
|
|
|
// @Param: STAB_TILT |
|
// @DisplayName: Stabilize mount's pitch/tilt angle |
|
// @Description: enable tilt/pitch stabilisation relative to Earth |
|
// @Values: 0:Disabled,1:Enabled |
|
// @User: Standard |
|
AP_GROUPINFO("STAB_TILT", 5, AP_Mount, _stab_tilt, 0), |
|
|
|
// @Param: STAB_PAN |
|
// @DisplayName: Stabilize mount pan/yaw angle |
|
// @Description: enable pan/yaw stabilisation relative to Earth |
|
// @Values: 0:Disabled,1:Enabled |
|
// @User: Standard |
|
AP_GROUPINFO("STAB_PAN", 6, AP_Mount, _stab_pan, 0), |
|
#endif |
|
|
|
// @Param: RC_IN_ROLL |
|
// @DisplayName: roll RC input channel |
|
// @Description: 0 for none, any other for the RC channel to be used to control roll movements |
|
// @Values: 0:Disabled,5:RC5,6:RC6,7:RC7,8:RC8 |
|
// @User: Standard |
|
AP_GROUPINFO("RC_IN_ROLL", 7, AP_Mount, _roll_rc_in, 0), |
|
|
|
// @Param: ANGMIN_ROL |
|
// @DisplayName: Minimum roll angle |
|
// @Description: Minimum physical roll angular position of mount. |
|
// @Units: Centi-Degrees |
|
// @Range: -18000 17999 |
|
// @Increment: 1 |
|
// @User: Standard |
|
AP_GROUPINFO("ANGMIN_ROL", 8, AP_Mount, _roll_angle_min, -4500), |
|
|
|
// @Param: ANGMAX_ROL |
|
// @DisplayName: Maximum roll angle |
|
// @Description: Maximum physical roll angular position of the mount |
|
// @Units: Centi-Degrees |
|
// @Range: -18000 17999 |
|
// @Increment: 1 |
|
// @User: Standard |
|
AP_GROUPINFO("ANGMAX_ROL", 9, AP_Mount, _roll_angle_max, 4500), |
|
|
|
// @Param: RC_IN_TILT |
|
// @DisplayName: tilt (pitch) RC input channel |
|
// @Description: 0 for none, any other for the RC channel to be used to control tilt (pitch) movements |
|
// @Values: 0:Disabled,5:RC5,6:RC6,7:RC7,8:RC8 |
|
// @User: Standard |
|
AP_GROUPINFO("RC_IN_TILT", 10, AP_Mount, _tilt_rc_in, 0), |
|
|
|
// @Param: ANGMIN_TIL |
|
// @DisplayName: Minimum tilt angle |
|
// @Description: Minimum physical tilt (pitch) angular position of mount. |
|
// @Units: Centi-Degrees |
|
// @Range: -18000 17999 |
|
// @Increment: 1 |
|
// @User: Standard |
|
AP_GROUPINFO("ANGMIN_TIL", 11, AP_Mount, _tilt_angle_min, -4500), |
|
|
|
// @Param: ANGMAX_TIL |
|
// @DisplayName: Maximum tilt angle |
|
// @Description: Maximum physical tilt (pitch) angular position of the mount |
|
// @Units: Centi-Degrees |
|
// @Range: -18000 17999 |
|
// @Increment: 1 |
|
// @User: Standard |
|
AP_GROUPINFO("ANGMAX_TIL", 12, AP_Mount, _tilt_angle_max, 4500), |
|
|
|
// @Param: RC_IN_PAN |
|
// @DisplayName: pan (yaw) RC input channel |
|
// @Description: 0 for none, any other for the RC channel to be used to control pan (yaw) movements |
|
// @Values: 0:Disabled,5:RC5,6:RC6,7:RC7,8:RC8 |
|
// @User: Standard |
|
AP_GROUPINFO("RC_IN_PAN", 13, AP_Mount, _pan_rc_in, 0), |
|
|
|
// @Param: ANGMIN_PAN |
|
// @DisplayName: Minimum pan angle |
|
// @Description: Minimum physical pan (yaw) angular position of mount. |
|
// @Units: Centi-Degrees |
|
// @Range: -18000 17999 |
|
// @Increment: 1 |
|
// @User: Standard |
|
AP_GROUPINFO("ANGMIN_PAN", 14, AP_Mount, _pan_angle_min, -4500), |
|
|
|
// @Param: ANGMAX_PAN |
|
// @DisplayName: Maximum pan angle |
|
// @Description: Maximum physical pan (yaw) angular position of the mount |
|
// @Units: Centi-Degrees |
|
// @Range: -18000 17999 |
|
// @Increment: 1 |
|
// @User: Standard |
|
AP_GROUPINFO("ANGMAX_PAN", 15, AP_Mount, _pan_angle_max, 4500), |
|
|
|
#if MNT_JSTICK_SPD_OPTION == ENABLED |
|
// @Param: JSTICK_SPD |
|
// @DisplayName: mount joystick speed |
|
// @Description: 0 for position control, small for low speeds, 100 for max speed. A good general value is 10 which gives a movement speed of 3 degrees per second. |
|
// @Range: 0 100 |
|
// @Increment: 1 |
|
// @User: Standard |
|
AP_GROUPINFO("JSTICK_SPD", 16, AP_Mount, _joystick_speed, 0), |
|
#endif |
|
|
|
AP_GROUPEND |
|
}; |
|
|
|
AP_Mount::AP_Mount(const struct Location *current_loc, GPS *&gps, const AP_AHRS &ahrs, uint8_t id) : |
|
_ahrs(ahrs), |
|
_gps(gps) |
|
{ |
|
AP_Param::setup_object_defaults(this, var_info); |
|
_current_loc = current_loc; |
|
|
|
// default to zero angles |
|
_retract_angles = Vector3f(0,0,0); |
|
_neutral_angles = Vector3f(0,0,0); |
|
_control_angles = Vector3f(0,0,0); |
|
|
|
// default unknown mount type |
|
_mount_type = k_unknown; |
|
|
|
#if MNT_MOUNT2_OPTION == ENABLED |
|
if (id == 0) { |
|
#endif |
|
_roll_idx = RC_Channel_aux::k_mount_roll; |
|
_tilt_idx = RC_Channel_aux::k_mount_tilt; |
|
_pan_idx = RC_Channel_aux::k_mount_pan; |
|
_open_idx = RC_Channel_aux::k_mount_open; |
|
#if MNT_MOUNT2_OPTION == ENABLED |
|
} else { |
|
_roll_idx = RC_Channel_aux::k_mount2_roll; |
|
_tilt_idx = RC_Channel_aux::k_mount2_tilt; |
|
_pan_idx = RC_Channel_aux::k_mount2_pan; |
|
_open_idx = RC_Channel_aux::k_mount2_open; |
|
} |
|
#endif |
|
} |
|
|
|
/// Auto-detect the mount gimbal type depending on the functions assigned to the servos |
|
void |
|
AP_Mount::update_mount_type() |
|
{ |
|
bool have_roll, have_tilt, have_pan; |
|
have_roll = RC_Channel_aux::function_assigned(RC_Channel_aux::k_mount_roll) || |
|
RC_Channel_aux::function_assigned(RC_Channel_aux::k_mount2_roll); |
|
have_tilt = RC_Channel_aux::function_assigned(RC_Channel_aux::k_mount_tilt) || |
|
RC_Channel_aux::function_assigned(RC_Channel_aux::k_mount2_tilt); |
|
have_pan = RC_Channel_aux::function_assigned(RC_Channel_aux::k_mount_pan) || |
|
RC_Channel_aux::function_assigned(RC_Channel_aux::k_mount2_pan); |
|
if (have_pan && have_tilt && !have_roll) { |
|
_mount_type = k_pan_tilt; |
|
} |
|
if (!have_pan && have_tilt && have_roll) { |
|
_mount_type = k_tilt_roll; |
|
} |
|
if (have_pan && have_tilt && have_roll) { |
|
_mount_type = k_pan_tilt_roll; |
|
} |
|
} |
|
|
|
/// sets the servo angles for retraction, note angles are in degrees |
|
void AP_Mount::set_retract_angles(float roll, float tilt, float pan) |
|
{ |
|
_retract_angles = Vector3f(roll, tilt, pan); |
|
} |
|
|
|
//sets the servo angles for neutral, note angles are in degrees |
|
void AP_Mount::set_neutral_angles(float roll, float tilt, float pan) |
|
{ |
|
_neutral_angles = Vector3f(roll, tilt, pan); |
|
} |
|
|
|
/// sets the servo angles for MAVLink, note angles are in degrees |
|
void AP_Mount::set_control_angles(float roll, float tilt, float pan) |
|
{ |
|
_control_angles = Vector3f(roll, tilt, pan); |
|
} |
|
|
|
/// used to tell the mount to track GPS location |
|
void AP_Mount::set_GPS_target_location(Location targetGPSLocation) |
|
{ |
|
_target_GPS_location=targetGPSLocation; |
|
} |
|
|
|
/// This one should be called periodically |
|
void AP_Mount::update_mount_position() |
|
{ |
|
#if MNT_RETRACT_OPTION == ENABLED |
|
static bool mount_open = 0; // 0 is closed |
|
#endif |
|
|
|
switch((enum MAV_MOUNT_MODE)_mount_mode.get()) |
|
{ |
|
#if MNT_RETRACT_OPTION == ENABLED |
|
// move mount to a "retracted position" or to a position where a fourth servo can retract the entire mount into the fuselage |
|
case MAV_MOUNT_MODE_RETRACT: |
|
{ |
|
Vector3f vec = _retract_angles.get(); |
|
_roll_angle = vec.x; |
|
_tilt_angle = vec.y; |
|
_pan_angle = vec.z; |
|
break; |
|
} |
|
#endif |
|
|
|
// move mount to a neutral position, typically pointing forward |
|
case MAV_MOUNT_MODE_NEUTRAL: |
|
{ |
|
Vector3f vec = _neutral_angles.get(); |
|
_roll_angle = vec.x; |
|
_tilt_angle = vec.y; |
|
_pan_angle = vec.z; |
|
break; |
|
} |
|
|
|
// point to the angles given by a mavlink message |
|
case MAV_MOUNT_MODE_MAVLINK_TARGETING: |
|
{ |
|
Vector3f vec = _control_angles.get(); |
|
_roll_control_angle = radians(vec.x); |
|
_tilt_control_angle = radians(vec.y); |
|
_pan_control_angle = radians(vec.z); |
|
stabilize(); |
|
break; |
|
} |
|
|
|
// RC radio manual angle control, but with stabilization from the AHRS |
|
case MAV_MOUNT_MODE_RC_TARGETING: |
|
{ |
|
#define rc_ch(i) RC_Channel::rc_channel(i-1) |
|
#if MNT_JSTICK_SPD_OPTION == ENABLED |
|
if (_joystick_speed) { // for spring loaded joysticks |
|
// allow pilot speed position input to come directly from an RC_Channel |
|
if (_roll_rc_in && rc_ch(_roll_rc_in)) { |
|
_roll_control_angle += rc_ch(_roll_rc_in)->norm_input() * 0.0001f * _joystick_speed; |
|
if (_roll_control_angle < radians(_roll_angle_min*0.01f)) _roll_control_angle = radians(_roll_angle_min*0.01f); |
|
if (_roll_control_angle > radians(_roll_angle_max*0.01f)) _roll_control_angle = radians(_roll_angle_max*0.01f); |
|
} |
|
if (_tilt_rc_in && (rc_ch(_tilt_rc_in))) { |
|
_tilt_control_angle += rc_ch(_tilt_rc_in)->norm_input() * 0.0001f * _joystick_speed; |
|
if (_tilt_control_angle < radians(_tilt_angle_min*0.01f)) _tilt_control_angle = radians(_tilt_angle_min*0.01f); |
|
if (_tilt_control_angle > radians(_tilt_angle_max*0.01f)) _tilt_control_angle = radians(_tilt_angle_max*0.01f); |
|
} |
|
if (_pan_rc_in && (rc_ch(_pan_rc_in))) { |
|
_pan_control_angle += rc_ch(_pan_rc_in)->norm_input() * 0.0001f * _joystick_speed; |
|
if (_pan_control_angle < radians(_pan_angle_min*0.01f)) _pan_control_angle = radians(_pan_angle_min*0.01f); |
|
if (_pan_control_angle > radians(_pan_angle_max*0.01f)) _pan_control_angle = radians(_pan_angle_max*0.01f); |
|
} |
|
} else { |
|
#endif |
|
// allow pilot position input to come directly from an RC_Channel |
|
if (_roll_rc_in && (rc_ch(_roll_rc_in))) { |
|
_roll_control_angle = angle_input_rad(rc_ch(_roll_rc_in), _roll_angle_min, _roll_angle_max); |
|
} |
|
if (_tilt_rc_in && (rc_ch(_tilt_rc_in))) { |
|
_tilt_control_angle = angle_input_rad(rc_ch(_tilt_rc_in), _tilt_angle_min, _tilt_angle_max); |
|
} |
|
if (_pan_rc_in && (rc_ch(_pan_rc_in))) { |
|
_pan_control_angle = angle_input_rad(rc_ch(_pan_rc_in), _pan_angle_min, _pan_angle_max); |
|
} |
|
#if MNT_JSTICK_SPD_OPTION == ENABLED |
|
} |
|
#endif |
|
stabilize(); |
|
break; |
|
} |
|
|
|
#if MNT_GPSPOINT_OPTION == ENABLED |
|
// point mount to a GPS point given by the mission planner |
|
case MAV_MOUNT_MODE_GPS_POINT: |
|
{ |
|
if(_gps->fix) { |
|
calc_GPS_target_angle(&_target_GPS_location); |
|
stabilize(); |
|
} |
|
break; |
|
} |
|
#endif |
|
|
|
default: |
|
//do nothing |
|
break; |
|
} |
|
|
|
#if MNT_RETRACT_OPTION == ENABLED |
|
// move mount to a "retracted position" into the fuselage with a fourth servo |
|
bool mount_open_new = (enum MAV_MOUNT_MODE)_mount_mode.get()==MAV_MOUNT_MODE_RETRACT ? 0 : 1; |
|
if (mount_open != mount_open_new) { |
|
mount_open = mount_open_new; |
|
move_servo(_open_idx, mount_open_new, 0, 1); |
|
} |
|
#endif |
|
|
|
// write the results to the servos |
|
move_servo(_roll_idx, _roll_angle*10, _roll_angle_min*0.1f, _roll_angle_max*0.1f); |
|
move_servo(_tilt_idx, _tilt_angle*10, _tilt_angle_min*0.1f, _tilt_angle_max*0.1f); |
|
move_servo(_pan_idx, _pan_angle*10, _pan_angle_min*0.1f, _pan_angle_max*0.1f); |
|
} |
|
|
|
void AP_Mount::set_mode(enum MAV_MOUNT_MODE mode) |
|
{ |
|
_mount_mode = (int8_t)mode; |
|
} |
|
|
|
/// Change the configuration of the mount |
|
/// triggered by a MavLink packet. |
|
void AP_Mount::configure_msg(mavlink_message_t* msg) |
|
{ |
|
__mavlink_mount_configure_t packet; |
|
mavlink_msg_mount_configure_decode(msg, &packet); |
|
if (mavlink_check_target(packet.target_system, packet.target_component)) { |
|
// not for us |
|
return; |
|
} |
|
set_mode((enum MAV_MOUNT_MODE)packet.mount_mode); |
|
_stab_roll = packet.stab_roll; |
|
_stab_tilt = packet.stab_pitch; |
|
_stab_pan = packet.stab_yaw; |
|
} |
|
|
|
/// Control the mount (depends on the previously set mount configuration) |
|
/// triggered by a MavLink packet. |
|
void AP_Mount::control_msg(mavlink_message_t *msg) |
|
{ |
|
__mavlink_mount_control_t packet; |
|
mavlink_msg_mount_control_decode(msg, &packet); |
|
if (mavlink_check_target(packet.target_system, packet.target_component)) { |
|
// not for us |
|
return; |
|
} |
|
|
|
switch ((enum MAV_MOUNT_MODE)_mount_mode.get()) |
|
{ |
|
#if MNT_RETRACT_OPTION == ENABLED |
|
case MAV_MOUNT_MODE_RETRACT: // Load and keep safe position (Roll,Pitch,Yaw) from EEPROM and stop stabilization |
|
set_retract_angles(packet.input_b*0.01f, packet.input_a*0.01f, packet.input_c*0.01f); |
|
if (packet.save_position) |
|
{ |
|
_retract_angles.save(); |
|
} |
|
break; |
|
#endif |
|
|
|
case MAV_MOUNT_MODE_NEUTRAL: // Load and keep neutral position (Roll,Pitch,Yaw) from EEPROM |
|
set_neutral_angles(packet.input_b*0.01f, packet.input_a*0.01f, packet.input_c*0.01f); |
|
if (packet.save_position) |
|
{ |
|
_neutral_angles.save(); |
|
} |
|
break; |
|
|
|
case MAV_MOUNT_MODE_MAVLINK_TARGETING: // Load neutral position and start MAVLink Roll,Pitch,Yaw control with stabilization |
|
set_control_angles(packet.input_b*0.01f, packet.input_a*0.01f, packet.input_c*0.01f); |
|
break; |
|
|
|
case MAV_MOUNT_MODE_RC_TARGETING: // Load neutral position and start RC Roll,Pitch,Yaw control with stabilization |
|
{ |
|
Vector3f vec = _neutral_angles.get(); |
|
_roll_angle = vec.x; |
|
_tilt_angle = vec.y; |
|
_pan_angle = vec.z; |
|
} |
|
break; |
|
|
|
#if MNT_GPSPOINT_OPTION == ENABLED |
|
case MAV_MOUNT_MODE_GPS_POINT: // Load neutral position and start to point to Lat,Lon,Alt |
|
Location targetGPSLocation; |
|
targetGPSLocation.lat = packet.input_a; |
|
targetGPSLocation.lng = packet.input_b; |
|
targetGPSLocation.alt = packet.input_c; |
|
set_GPS_target_location(targetGPSLocation); |
|
break; |
|
#endif |
|
|
|
case MAV_MOUNT_MODE_ENUM_END: |
|
break; |
|
|
|
default: |
|
// do nothing |
|
break; |
|
} |
|
} |
|
|
|
/// Return mount status information (depends on the previously set mount configuration) |
|
/// triggered by a MavLink packet. |
|
void AP_Mount::status_msg(mavlink_message_t *msg) |
|
{ |
|
__mavlink_mount_status_t packet; |
|
mavlink_msg_mount_status_decode(msg, &packet); |
|
if (mavlink_check_target(packet.target_system, packet.target_component)) { |
|
// not for us |
|
return; |
|
} |
|
|
|
switch ((enum MAV_MOUNT_MODE)_mount_mode.get()) |
|
{ |
|
case MAV_MOUNT_MODE_RETRACT: // safe position (Roll,Pitch,Yaw) from EEPROM and stop stabilization |
|
case MAV_MOUNT_MODE_NEUTRAL: // neutral position (Roll,Pitch,Yaw) from EEPROM |
|
case MAV_MOUNT_MODE_MAVLINK_TARGETING: // neutral position and start MAVLink Roll,Pitch,Yaw control with stabilization |
|
case MAV_MOUNT_MODE_RC_TARGETING: // neutral position and start RC Roll,Pitch,Yaw control with stabilization |
|
packet.pointing_b = _roll_angle*100; // degrees*100 |
|
packet.pointing_a = _tilt_angle*100; // degrees*100 |
|
packet.pointing_c = _pan_angle*100; // degrees*100 |
|
break; |
|
#if MNT_GPSPOINT_OPTION == ENABLED |
|
case MAV_MOUNT_MODE_GPS_POINT: // neutral position and start to point to Lat,Lon,Alt |
|
packet.pointing_a = _target_GPS_location.lat; // latitude |
|
packet.pointing_b = _target_GPS_location.lng; // longitude |
|
packet.pointing_c = _target_GPS_location.alt; // altitude |
|
break; |
|
#endif |
|
case MAV_MOUNT_MODE_ENUM_END: |
|
break; |
|
} |
|
|
|
// status reply |
|
// TODO: is COMM_3 correct ? |
|
mavlink_msg_mount_status_send(MAVLINK_COMM_3, packet.target_system, packet.target_component, |
|
packet.pointing_a, packet.pointing_b, packet.pointing_c); |
|
} |
|
|
|
/// Set mount point/region of interest, triggered by mission script commands |
|
void AP_Mount::set_roi_cmd(const struct Location *target_loc) |
|
{ |
|
#if MNT_GPSPOINT_OPTION == ENABLED |
|
// set the target gps location |
|
_target_GPS_location = *target_loc; |
|
|
|
// set the mode to GPS tracking mode |
|
set_mode(MAV_MOUNT_MODE_GPS_POINT); |
|
#endif |
|
} |
|
|
|
/// Set mount configuration, triggered by mission script commands |
|
void AP_Mount::configure_cmd() |
|
{ |
|
// TODO get the information out of the mission command and use it |
|
} |
|
|
|
/// Control the mount (depends on the previously set mount configuration), triggered by mission script commands |
|
void AP_Mount::control_cmd() |
|
{ |
|
// TODO get the information out of the mission command and use it |
|
} |
|
|
|
/// returns the angle (degrees*100) that the RC_Channel input is receiving |
|
int32_t |
|
AP_Mount::angle_input(RC_Channel* rc, int16_t angle_min, int16_t angle_max) |
|
{ |
|
return (rc->get_reverse() ? -1 : 1) * (rc->radio_in - rc->radio_min) * (int32_t)(angle_max - angle_min) / (rc->radio_max - rc->radio_min) + (rc->get_reverse() ? angle_max : angle_min); |
|
} |
|
|
|
/// returns the angle (radians) that the RC_Channel input is receiving |
|
float |
|
AP_Mount::angle_input_rad(RC_Channel* rc, int16_t angle_min, int16_t angle_max) |
|
{ |
|
return radians(angle_input(rc, angle_min, angle_max)*0.01f); |
|
} |
|
|
|
void |
|
AP_Mount::calc_GPS_target_angle(const struct Location *target) |
|
{ |
|
float GPS_vector_x = (target->lng-_current_loc->lng)*cosf(ToRad((_current_loc->lat+target->lat)*0.00000005f))*0.01113195f; |
|
float GPS_vector_y = (target->lat-_current_loc->lat)*0.01113195f; |
|
float GPS_vector_z = (target->alt-_current_loc->alt); // baro altitude(IN CM) should be adjusted to known home elevation before take off (Set altimeter). |
|
float target_distance = 100.0f*pythagorous2(GPS_vector_x, GPS_vector_y); // Careful , centimeters here locally. Baro/alt is in cm, lat/lon is in meters. |
|
_roll_control_angle = 0; |
|
_tilt_control_angle = atan2f(GPS_vector_z, target_distance); |
|
_pan_control_angle = atan2f(GPS_vector_x, GPS_vector_y); |
|
} |
|
|
|
/// Stabilizes mount relative to the Earth's frame |
|
/// Inputs: |
|
/// _roll_control_angle desired roll angle in radians, |
|
/// _tilt_control_angle desired tilt/pitch angle in radians, |
|
/// _pan_control_angle desired pan/yaw angle in radians |
|
/// Outputs: |
|
/// _roll_angle stabilized roll angle in degrees, |
|
/// _tilt_angle stabilized tilt/pitch angle in degrees, |
|
/// _pan_angle stabilized pan/yaw angle in degrees |
|
void |
|
AP_Mount::stabilize() |
|
{ |
|
#if MNT_STABILIZE_OPTION == ENABLED |
|
// only do the full 3D frame transform if we are doing pan control |
|
if (_stab_pan) { |
|
Matrix3f m; ///< holds 3 x 3 matrix, var is used as temp in calcs |
|
Matrix3f cam; ///< Rotation matrix earth to camera. Desired camera from input. |
|
Matrix3f gimbal_target; ///< Rotation matrix from plane to camera. Then Euler angles to the servos. |
|
m = _ahrs.get_dcm_matrix(); |
|
m.transpose(); |
|
cam.from_euler(_roll_control_angle, _tilt_control_angle, _pan_control_angle); |
|
gimbal_target = m * cam; |
|
gimbal_target.to_euler(&_roll_angle, &_tilt_angle, &_pan_angle); |
|
_roll_angle = _stab_roll ? degrees(_roll_angle) : degrees(_roll_control_angle); |
|
_tilt_angle = _stab_tilt ? degrees(_tilt_angle) : degrees(_tilt_control_angle); |
|
_pan_angle = degrees(_pan_angle); |
|
} else { |
|
// otherwise base mount roll and tilt on the ahrs |
|
// roll/tilt attitude, plus any requested angle |
|
_roll_angle = degrees(_roll_control_angle); |
|
_tilt_angle = degrees(_tilt_control_angle); |
|
_pan_angle = degrees(_pan_control_angle); |
|
if (_stab_roll) { |
|
_roll_angle -= degrees(_ahrs.roll); |
|
} |
|
if (_stab_tilt) { |
|
_tilt_angle -= degrees(_ahrs.pitch); |
|
} |
|
} |
|
#endif |
|
} |
|
/* |
|
* /// For testing and development. Called in the medium loop. |
|
* void |
|
* AP_Mount::debug_output() |
|
* { Serial3.print("current - "); |
|
* Serial3.print("lat "); |
|
* Serial3.print(_current_loc->lat); |
|
* Serial3.print(",lon "); |
|
* Serial3.print(_current_loc->lng); |
|
* Serial3.print(",alt "); |
|
* Serial3.println(_current_loc->alt); |
|
* |
|
* Serial3.print("gps - "); |
|
* Serial3.print("lat "); |
|
* Serial3.print(_gps->latitude); |
|
* Serial3.print(",lon "); |
|
* Serial3.print(_gps->longitude); |
|
* Serial3.print(",alt "); |
|
* Serial3.print(_gps->altitude); |
|
* Serial3.println(); |
|
* |
|
* Serial3.print("target - "); |
|
* Serial3.print("lat "); |
|
* Serial3.print(_target_GPS_location.lat); |
|
* Serial3.print(",lon "); |
|
* Serial3.print(_target_GPS_location.lng); |
|
* Serial3.print(",alt "); |
|
* Serial3.print(_target_GPS_location.alt); |
|
* Serial3.print(" hdg to targ "); |
|
* Serial3.print(degrees(_pan_control_angle)); |
|
* Serial3.println(); |
|
* } |
|
*/ |
|
/// saturate to the closest angle limit if outside of [min max] angle interval |
|
/// input angle is in degrees * 10 |
|
int16_t |
|
AP_Mount::closest_limit(int16_t angle, int16_t* angle_min, int16_t* angle_max) |
|
{ |
|
// Make sure the angle lies in the interval [-180 .. 180[ degrees |
|
while (angle < -1800) angle += 3600; |
|
while (angle >= 1800) angle -= 3600; |
|
|
|
// Make sure the angle limits lie in the interval [-180 .. 180[ degrees |
|
while (*angle_min < -1800) *angle_min += 3600; |
|
while (*angle_min >= 1800) *angle_min -= 3600; |
|
while (*angle_max < -1800) *angle_max += 3600; |
|
while (*angle_max >= 1800) *angle_max -= 3600; |
|
// TODO call this function somehow, otherwise this will never work |
|
//set_range(min, max); |
|
|
|
// If the angle is outside servo limits, saturate the angle to the closest limit |
|
// On a circle the closest angular position must be carefully calculated to account for wrap-around |
|
if ((angle < *angle_min) && (angle > *angle_max)) { |
|
// angle error if min limit is used |
|
int16_t err_min = *angle_min - angle + (angle<*angle_min ? 0 : 3600); // add 360 degrees if on the "wrong side" |
|
// angle error if max limit is used |
|
int16_t err_max = angle - *angle_max + (angle>*angle_max ? 0 : 3600); // add 360 degrees if on the "wrong side" |
|
angle = err_min<err_max ? *angle_min : *angle_max; |
|
} |
|
|
|
return angle; |
|
} |
|
|
|
/// all angles are degrees * 10 units |
|
void |
|
AP_Mount::move_servo(uint8_t function_idx, int16_t angle, int16_t angle_min, int16_t angle_max) |
|
{ |
|
// saturate to the closest angle limit if outside of [min max] angle interval |
|
int16_t servo_out = closest_limit(angle, &angle_min, &angle_max); |
|
RC_Channel_aux::move_servo((RC_Channel_aux::Aux_servo_function_t)function_idx, servo_out, angle_min, angle_max); |
|
}
|
|
|