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px4-firmware/posix-configs/SITL/init/test/test_shutdown

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add simple SITL shutdown test
2018-11-16 13:13:57 -04:00
#!/bin/sh
# PX4 commands need the 'px4-' prefix in bash.
# (px4-alias.sh is expected to be in the PATH)
. px4-alias.sh
uorb start
param load
param set BAT_N_CELLS 3
commander: reboot/shutdown usability fixes - always check with state machine before reboot/shutdown - respect BOARD_HAS_POWER_CONTROL (shutdown from command, low battery, power button) - px4_shutdown_request add optional delay and always execute from HPWORK - px4_shutdown_request split out px4_reboot_request
2020-05-04 13:33:31 -03:00
param set CBRK_SUPPLY_CHK 894281
add simple SITL shutdown test
2018-11-16 13:13:57 -04:00
param set MAV_TYPE 22
param set VT_TYPE 2
param set SYS_RESTART_TYPE 0
dataman start
simulator move to PX4Accelerometer, PX4Gyroscope, PX4Magnetometer, PX4Barometer helpers (#12081)
2019-05-30 22:07:26 -03:00
simulator start
add simple SITL shutdown test
2018-11-16 13:13:57 -04:00
tone_alarm start
pwm_out_sim start
sensors split rc_update into new standalone module
2019-11-24 14:25:11 -04:00
rc_update start
add simple SITL shutdown test
2018-11-16 13:13:57 -04:00
sensors start
commander start
land_detector start vtol
navigator start
ekf2 start
vtol_att_control start
move hover_thrust_estimator to new module (mc_hover_thrust_estimator) * MC_HTE: unitialize with hover_thrust parameter * MC_HTE: constrain hover thrust setter between 0.1 and 0.9 * MC_HTE: integrate with land detector and velocity controller * MCHoverThrustEstimator: Always publish an estimate even when not fusing measurements. This is required as the land detector and the position controller need to receive a hover thrust value. * MC_HTE: use altitude agl threshold to start the estimator local_position.z is relative to the origin of the EKF while dist_bottom is above ground Co-authored-by: bresch <brescianimathieu@gmail.com>
2020-03-11 22:20:54 -03:00
mc_hover_thrust_estimator start
VTOL: explicitly start all FW & MC controllers in VTOL mode
2019-11-30 13:58:36 -04:00
mc_pos_control start vtol
mc_att_control start vtol
mc_rate_control start vtol
fw_pos_control_l1 start vtol
fw_att_control start vtol
Airspeed Selector: repurpose wind estimator into an airspeed (selection, validation) module. This new airspeed module does: -runns an airspeed validator for every airspeed sensor present, which checks measurement validity and estimates an airspeed scale -selects another airspeed sensor if for the current one a failure is detected -estimates airspeed with groundspeed-windspeed if no valid airspeed sensor is present -outputs airspeed_validated topic Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2019-08-07 08:06:00 -03:00
airspeed_selector start
add simple SITL shutdown test
2018-11-16 13:13:57 -04:00
#mixer load /dev/pwm_output0 ROMFS/sitl/mixers/standard_vtol_sitl.main.mix
ver all
logger start -e -t
mavlink boot_complete
commander: reboot/shutdown usability fixes - always check with state machine before reboot/shutdown - respect BOARD_HAS_POWER_CONTROL (shutdown from command, low battery, power button) - px4_shutdown_request add optional delay and always execute from HPWORK - px4_shutdown_request split out px4_reboot_request
2020-05-04 13:33:31 -03:00
sleep 1
add simple SITL shutdown test
2018-11-16 13:13:57 -04:00
echo "Boot complete"
# status of all running modules
echo "Checking status of all modules"
logger status
pwm_out_sim status
sensors status
commander status
sensors split rc_update into new standalone module
2019-11-24 14:25:11 -04:00
rc_update stop
add simple SITL shutdown test
2018-11-16 13:13:57 -04:00
land_detector status
navigator status
ekf2 status
mc_pos_control status
mc_att_control status
create new multicopter rate controller module (mc_rate_control) split out of mc_att_control
2019-11-19 18:03:11 -04:00
mc_rate_control status
add simple SITL shutdown test
2018-11-16 13:13:57 -04:00
fw_pos_control_l1 status
fw_att_control status
Airspeed Selector: repurpose wind estimator into an airspeed (selection, validation) module. This new airspeed module does: -runns an airspeed validator for every airspeed sensor present, which checks measurement validity and estimates an airspeed scale -selects another airspeed sensor if for the current one a failure is detected -estimates airspeed with groundspeed-windspeed if no valid airspeed sensor is present -outputs airspeed_validated topic Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2019-08-07 08:06:00 -03:00
airspeed_selector status
add simple SITL shutdown test
2018-11-16 13:13:57 -04:00
dataman status
uorb status
# stop all
echo "Stopping all modules"
logger stop
pwm_out_sim stop
create new multicopter rate controller module (mc_rate_control) split out of mc_att_control
2019-11-19 18:03:11 -04:00
mc_rate_control stop
add simple SITL shutdown test
2018-11-16 13:13:57 -04:00
mc_att_control stop
fw_att_control stop
mc_pos_control stop
fw_pos_control_l1 stop
navigator stop
commander stop
land_detector stop
ekf2 stop
Airspeed Selector: repurpose wind estimator into an airspeed (selection, validation) module. This new airspeed module does: -runns an airspeed validator for every airspeed sensor present, which checks measurement validity and estimates an airspeed scale -selects another airspeed sensor if for the current one a failure is detected -estimates airspeed with groundspeed-windspeed if no valid airspeed sensor is present -outputs airspeed_validated topic Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2019-08-07 08:06:00 -03:00
airspeed_selector stop
add simple SITL shutdown test
2018-11-16 13:13:57 -04:00
sensors stop
simulator stop
tone_alarm stop
dataman stop
#uorb stop
shutdown