2015-06-04 00:13:34 -03:00
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/*
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additional arming checks for plane
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*/
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2017-01-09 03:56:56 -04:00
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#include "AP_Arming.h"
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2015-06-04 00:13:34 -03:00
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#include "Plane.h"
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2015-10-25 14:03:46 -03:00
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const AP_Param::GroupInfo AP_Arming_Plane::var_info[] = {
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2015-08-24 00:53:15 -03:00
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// variables from parent vehicle
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AP_NESTEDGROUPINFO(AP_Arming, 0),
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2018-09-08 00:35:18 -03:00
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// index 3 was RUDDER and should not be used
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2015-08-24 00:53:15 -03:00
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AP_GROUPEND
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};
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2015-06-04 00:13:34 -03:00
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/*
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additional arming checks for plane
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2016-11-05 20:23:32 -03:00
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2015-06-04 00:13:34 -03:00
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*/
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2017-08-09 08:22:15 -03:00
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bool AP_Arming_Plane::pre_arm_checks(bool display_failure)
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2015-06-04 00:13:34 -03:00
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{
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// call parent class checks
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2017-08-09 08:22:15 -03:00
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bool ret = AP_Arming::pre_arm_checks(display_failure);
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2015-06-04 00:13:34 -03:00
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2015-08-24 00:53:15 -03:00
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// Check airspeed sensor
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2017-08-09 08:22:15 -03:00
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ret &= AP_Arming::airspeed_checks(display_failure);
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2015-08-24 00:53:15 -03:00
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2017-12-06 19:02:11 -04:00
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if (plane.g.fs_timeout_long < plane.g.fs_timeout_short && plane.g.fs_action_short != FS_ACTION_SHORT_DISABLED) {
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2017-08-09 08:22:15 -03:00
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check_failed(ARMING_CHECK_NONE, display_failure, "FS_LONG_TIMEOUT < FS_SHORT_TIMEOUT");
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2017-09-19 23:18:37 -03:00
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ret = false;
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}
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2016-06-23 09:40:13 -03:00
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if (plane.aparm.roll_limit_cd < 300) {
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2017-08-09 08:22:15 -03:00
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check_failed(ARMING_CHECK_NONE, display_failure, "LIM_ROLL_CD too small (%u)", plane.aparm.roll_limit_cd);
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ret = false;
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2015-06-04 00:13:34 -03:00
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}
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if (plane.aparm.pitch_limit_max_cd < 300) {
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2017-08-09 08:22:15 -03:00
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check_failed(ARMING_CHECK_NONE, display_failure, "LIM_PITCH_MAX too small (%u)", plane.aparm.pitch_limit_max_cd);
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ret = false;
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2015-06-04 00:13:34 -03:00
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}
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if (plane.aparm.pitch_limit_min_cd > -300) {
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2017-08-09 08:22:15 -03:00
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check_failed(ARMING_CHECK_NONE, display_failure, "LIM_PITCH_MIN too large (%u)", plane.aparm.pitch_limit_min_cd);
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ret = false;
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2015-06-04 00:13:34 -03:00
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}
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if (plane.channel_throttle->get_reverse() &&
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plane.g.throttle_fs_enabled &&
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plane.g.throttle_fs_value <
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ArduPlane: Fix up after refactoring RC_Channel class
Further to refactor of RC_Channel class which included
adding get_xx set_xx methods, change reads and writes to the public members
to calls to get and set functionsss
old public member(int16_t) get function -> int16_t set function (int16_t)
(expression where c is an object of type RC_Channel)
c.radio_in c.get_radio_in() c.set_radio_in(v)
c.control_in c.get_control_in() c.set_control_in(v)
c.servo_out c.get_servo_out() c.set_servo_out(v)
c.pwm_out c.get_pwm_out() // use existing
c.radio_out c.get_radio_out() c.set_radio_out(v)
c.radio_max c.get_radio_max() c.set_radio_max(v)
c.radio_min c.get_radio_min() c.set_radio_min(v)
c.radio_trim c.get_radio_trim() c.set_radio_trim(v);
c.min_max_configured() // return true if min and max are configured
Because data members of RC_Channels are now private and so cannot be written directly
some overloads are provided in the Plane classes to provide the old functionality
new overload Plane::stick_mix_channel(RC_Channel *channel)
which forwards to the previously existing
void stick_mix_channel(RC_Channel *channel, int16_t &servo_out);
new overload Plane::channel_output_mixer(Rc_Channel* , RC_Channel*)const
which forwards to
(uint8_t mixing_type, int16_t & chan1, int16_t & chan2)const;
Rename functions
RC_Channel_aux::set_radio_trim(Aux_servo_function_t function)
to RC_Channel_aux::set_trim_to_radio_in_for(Aux_servo_function_t function)
RC_Channel_aux::set_servo_out(Aux_servo_function_t function, int16_t value)
to RC_Channel_aux::set_servo_out_for(Aux_servo_function_t function, int16_t value)
Rationale:
RC_Channel is a complicated class, which combines
several functionalities dealing with stick inputs
in pwm and logical units, logical and actual actuator
outputs, unit conversion etc, etc
The intent of this PR is to clarify existing use of
the class. At the basic level it should now be possible
to grep all places where private variable is set by
searching for the set_xx function.
(The wider purpose is to provide a more generic and
logically simpler method of output mixing. This is a small step)
2016-05-08 05:33:02 -03:00
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plane.channel_throttle->get_radio_max()) {
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2017-08-09 08:22:15 -03:00
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check_failed(ARMING_CHECK_NONE, display_failure, "Invalid THR_FS_VALUE for rev throttle");
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2015-06-04 00:13:34 -03:00
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ret = false;
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}
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2016-02-20 05:02:52 -04:00
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if (plane.quadplane.available() && plane.scheduler.get_loop_rate_hz() < 100) {
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2017-08-09 08:22:15 -03:00
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check_failed(ARMING_CHECK_NONE, display_failure, "quadplane needs SCHED_LOOP_RATE >= 100");
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2016-02-20 05:02:52 -04:00
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ret = false;
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}
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2016-02-21 12:06:43 -04:00
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if (plane.control_mode == AUTO && plane.mission.num_commands() <= 1) {
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2017-08-09 08:22:15 -03:00
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check_failed(ARMING_CHECK_NONE, display_failure, "No mission loaded");
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2016-02-21 12:06:43 -04:00
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ret = false;
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}
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2016-08-12 17:02:31 -03:00
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// check adsb avoidance failsafe
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if (plane.failsafe.adsb) {
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2017-08-09 08:22:15 -03:00
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check_failed(ARMING_CHECK_NONE, display_failure, "ADSB threat detected");
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2016-08-12 17:02:31 -03:00
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ret = false;
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}
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2016-09-10 19:19:22 -03:00
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#if HAVE_PX4_MIXER
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2016-09-06 04:03:13 -03:00
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if (plane.last_mixer_crc == -1) {
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2017-08-09 08:22:15 -03:00
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check_failed(ARMING_CHECK_NONE, display_failure, "Mixer error");
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2016-09-06 04:03:13 -03:00
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ret = false;
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}
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#endif // CONFIG_HAL_BOARD
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2015-06-04 00:13:34 -03:00
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return ret;
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}
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2015-10-16 00:52:57 -03:00
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2017-08-09 08:22:15 -03:00
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bool AP_Arming_Plane::ins_checks(bool display_failure)
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2015-10-16 00:52:57 -03:00
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{
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// call parent class checks
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2017-08-09 08:22:15 -03:00
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if (!AP_Arming::ins_checks(display_failure)) {
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2015-10-16 00:52:57 -03:00
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return false;
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}
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// additional plane specific checks
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if ((checks_to_perform & ARMING_CHECK_ALL) ||
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(checks_to_perform & ARMING_CHECK_INS)) {
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2018-06-25 02:44:04 -03:00
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if (!AP::ahrs().healthy()) {
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const char *reason = AP::ahrs().prearm_failure_reason();
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2017-08-09 08:22:15 -03:00
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if (reason == nullptr) {
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reason = "AHRS not healthy";
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2015-10-16 00:52:57 -03:00
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}
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2017-08-09 08:22:15 -03:00
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check_failed(ARMING_CHECK_INS, display_failure, "%s", reason);
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2015-10-16 00:52:57 -03:00
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return false;
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}
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}
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return true;
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}
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