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author | Lorenz Meier <lm@inf.ethz.ch> | 2012-12-27 18:27:08 +0100 |
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committer | Lorenz Meier <lm@inf.ethz.ch> | 2012-12-27 18:27:08 +0100 |
commit | f5bad08bd0f4e0f6506deeac9d369b2b9c2d9e32 (patch) | |
tree | 9da695a79082b70360260c669f27ff8fa4470b35 /apps/multirotor_att_control | |
parent | 61d7e1d28552ddd7652b1d1b888c51a2eae78967 (diff) | |
download | px4-firmware-f5bad08bd0f4e0f6506deeac9d369b2b9c2d9e32.tar.gz px4-firmware-f5bad08bd0f4e0f6506deeac9d369b2b9c2d9e32.tar.bz2 px4-firmware-f5bad08bd0f4e0f6506deeac9d369b2b9c2d9e32.zip |
Cleaned up control mode state machine / flight mode / navigation state machine still needs a bit cleaning up
Diffstat (limited to 'apps/multirotor_att_control')
-rw-r--r-- | apps/multirotor_att_control/multirotor_att_control_main.c | 87 |
1 files changed, 51 insertions, 36 deletions
diff --git a/apps/multirotor_att_control/multirotor_att_control_main.c b/apps/multirotor_att_control/multirotor_att_control_main.c index ce1e52c1b..f184859a3 100644 --- a/apps/multirotor_att_control/multirotor_att_control_main.c +++ b/apps/multirotor_att_control/multirotor_att_control_main.c @@ -232,19 +232,9 @@ mc_thread_main(int argc, char *argv[]) /* STEP 2: publish the result to the vehicle actuators */ orb_publish(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, &att_sp); } - /* decide wether we want rate or position input */ - } - else if (state.flag_control_manual_enabled) { - - /* manual inputs, from RC control or joystick */ - if (state.flag_control_rates_enabled && !state.flag_control_attitude_enabled) { - rates_sp.roll = manual.roll; + - rates_sp.pitch = manual.pitch; - rates_sp.yaw = manual.yaw; - rates_sp.thrust = manual.throttle; - rates_sp.timestamp = hrt_absolute_time(); - } + } else if (state.flag_control_manual_enabled) { if (state.flag_control_attitude_enabled) { @@ -258,7 +248,7 @@ mc_thread_main(int argc, char *argv[]) static bool rc_loss_first_time = true; /* if the RC signal is lost, try to stay level and go slowly back down to ground */ - if(state.rc_signal_lost) { + if (state.rc_signal_lost) { /* the failsafe throttle is stored as a parameter, as it depends on the copter and the payload */ param_get(failsafe_throttle_handle, &failsafe_throttle); att_sp.roll_body = 0.0f; @@ -285,41 +275,66 @@ mc_thread_main(int argc, char *argv[]) att_sp.yaw_body = att.yaw; } - /* only move setpoint if manual input is != 0 */ + /* act if stabilization is active or if the (nonsense) direct pass through mode is set */ + if (state.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_SAS || + state.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_DIRECT) { - if(manual.mode == MANUAL_CONTROL_MODE_ATT_YAW_POS) { - if ((manual.yaw < -0.01f || 0.01f < manual.yaw) && manual.throttle > 0.3f) { + if (state.manual_sas_mode == VEHICLE_MANUAL_SAS_MODE_ROLL_PITCH_ABS_YAW_RATE) { rates_sp.yaw = manual.yaw; control_yaw_position = false; - first_time_after_yaw_speed_control = true; } else { - if (first_time_after_yaw_speed_control) { - att_sp.yaw_body = att.yaw; - first_time_after_yaw_speed_control = false; + /* + * This mode SHOULD be the default mode, which is: + * VEHICLE_MANUAL_SAS_MODE_ROLL_PITCH_ABS_YAW_ABS + * + * However, we fall back to this setting for all other (nonsense) + * settings as well. + */ + + /* only move setpoint if manual input is != 0 */ + if ((manual.yaw < -0.01f || 0.01f < manual.yaw) && manual.throttle > 0.3f) { + rates_sp.yaw = manual.yaw; + control_yaw_position = false; + first_time_after_yaw_speed_control = true; + } else { + if (first_time_after_yaw_speed_control) { + att_sp.yaw_body = att.yaw; + first_time_after_yaw_speed_control = false; + } + control_yaw_position = true; } - control_yaw_position = true; } - } else if (manual.mode == MANUAL_CONTROL_MODE_ATT_YAW_RATE) { - rates_sp.yaw = manual.yaw; - control_yaw_position = false; } att_sp.thrust = manual.throttle; att_sp.timestamp = hrt_absolute_time(); } - } - /* STEP 2: publish the result to the vehicle actuators */ - orb_publish(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, &att_sp); - - if (motor_test_mode) { - printf("testmode"); - att_sp.roll_body = 0.0f; - att_sp.pitch_body = 0.0f; - att_sp.yaw_body = 0.0f; - att_sp.thrust = 0.1f; - att_sp.timestamp = hrt_absolute_time(); - /* STEP 2: publish the result to the vehicle actuators */ + + /* STEP 2: publish the controller output */ orb_publish(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, &att_sp); + + if (motor_test_mode) { + printf("testmode"); + att_sp.roll_body = 0.0f; + att_sp.pitch_body = 0.0f; + att_sp.yaw_body = 0.0f; + att_sp.thrust = 0.1f; + att_sp.timestamp = hrt_absolute_time(); + /* STEP 2: publish the result to the vehicle actuators */ + orb_publish(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, &att_sp); + } + + } else { + /* manual rate inputs, from RC control or joystick */ + if (state.flag_control_rates_enabled && + state.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_RATES) { + rates_sp.roll = manual.roll; + + rates_sp.pitch = manual.pitch; + rates_sp.yaw = manual.yaw; + rates_sp.thrust = manual.throttle; + rates_sp.timestamp = hrt_absolute_time(); + } } } |