Plane: move arming-related functionality into parent classes

Logging moves up
arming via mavlink moves up
arming via switch moves up
This commit is contained in:
Peter Barker 2019-05-04 09:35:12 +10:00 committed by Randy Mackay
parent 9851ec1ddb
commit 400aa53654
14 changed files with 35 additions and 88 deletions

View File

@ -24,7 +24,14 @@ public:
// var_info for holding Parameter information
static const struct AP_Param::GroupInfo var_info[];
bool disarm() override;
bool arm(AP_Arming::Method method, bool do_arming_checks=true) override;
void update_soft_armed();
protected:
bool ins_checks(bool report) override;
private:
void change_arm_state(void);
};

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@ -129,17 +129,17 @@ void Plane::loop()
G_Dt = scheduler.get_loop_period_s();
}
void Plane::update_soft_armed()
void AP_Arming_Plane::update_soft_armed()
{
hal.util->set_soft_armed(arming.is_armed() &&
hal.util->set_soft_armed(is_armed() &&
hal.util->safety_switch_state() != AP_HAL::Util::SAFETY_DISARMED);
logger.set_vehicle_armed(hal.util->get_soft_armed());
AP::logger().set_vehicle_armed(hal.util->get_soft_armed());
}
// update AHRS system
void Plane::ahrs_update()
{
update_soft_armed();
arming.update_soft_armed();
#if HIL_SUPPORT
if (g.hil_mode == 1) {
@ -668,7 +668,7 @@ void Plane::disarm_if_autoland_complete()
arming.is_armed()) {
/* we have auto disarm enabled. See if enough time has passed */
if (millis() - auto_state.last_flying_ms >= landing.get_disarm_delay()*1000UL) {
if (disarm_motors()) {
if (arming.disarm()) {
gcs().send_text(MAV_SEVERITY_INFO,"Auto disarmed");
}
}

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@ -851,22 +851,6 @@ MAV_RESULT GCS_MAVLINK_Plane::handle_command_long_packet(const mavlink_command_l
plane.set_mode(plane.mode_auto, MODE_REASON_GCS_COMMAND);
return MAV_RESULT_ACCEPTED;
case MAV_CMD_COMPONENT_ARM_DISARM:
if (is_equal(packet.param1,1.0f)) {
// run pre_arm_checks and arm_checks and display failures
const bool do_arming_checks = !is_equal(packet.param2,magic_force_arm_value);
if (plane.arm_motors(AP_Arming::Method::MAVLINK, do_arming_checks)) {
return MAV_RESULT_ACCEPTED;
}
return MAV_RESULT_FAILED;
} else if (is_zero(packet.param1)) {
if (plane.disarm_motors()) {
return MAV_RESULT_ACCEPTED;
}
return MAV_RESULT_FAILED;
}
return MAV_RESULT_UNSUPPORTED;
case MAV_CMD_DO_LAND_START:
// attempt to switch to next DO_LAND_START command in the mission
if (plane.mission.jump_to_landing_sequence()) {

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@ -210,24 +210,6 @@ void Plane::Log_Write_Sonar()
logger.WriteBlock(&pkt, sizeof(pkt));
}
struct PACKED log_Arm_Disarm {
LOG_PACKET_HEADER;
uint64_t time_us;
uint8_t arm_state;
uint16_t arm_checks;
};
void Plane::Log_Arm_Disarm() {
struct log_Arm_Disarm pkt = {
LOG_PACKET_HEADER_INIT(LOG_ARM_DISARM_MSG),
time_us : AP_HAL::micros64(),
arm_state : arming.is_armed(),
arm_checks : arming.get_enabled_checks()
};
logger.WriteCriticalBlock(&pkt, sizeof(pkt));
}
struct PACKED log_AETR {
LOG_PACKET_HEADER;
uint64_t time_us;
@ -276,8 +258,6 @@ const struct LogStructure Plane::log_structure[] = {
"NTUN", "QfcccfffLLii", "TimeUS,Dist,TBrg,NavBrg,AltErr,XT,XTi,AspdE,TLat,TLng,TAlt,TAspd", "smddmmmnDUmn", "F0BBB0B0GGBB" },
{ LOG_SONAR_MSG, sizeof(log_Sonar),
"SONR", "QffBf", "TimeUS,Dist,Volt,Cnt,Corr", "smv--", "FB0--" },
{ LOG_ARM_DISARM_MSG, sizeof(log_Arm_Disarm),
"ARM", "QBH", "TimeUS,ArmState,ArmChecks", "s--", "F--" },
{ LOG_ATRP_MSG, sizeof(AP_AutoTune::log_ATRP),
"ATRP", "QBBcfff", "TimeUS,Type,State,Servo,Demanded,Achieved,P", "s---dd-", "F---00-" },
{ LOG_STATUS_MSG, sizeof(log_Status),
@ -326,7 +306,6 @@ void Plane::Log_Write_Nav_Tuning() {}
void Plane::Log_Write_Status() {}
void Plane::Log_Write_Sonar() {}
void Plane::Log_Arm_Disarm() {}
void Plane::Log_Write_RC(void) {}
void Plane::Log_Write_Vehicle_Startup_Messages() {}

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@ -829,7 +829,6 @@ private:
void Log_Write_Nav_Tuning();
void Log_Write_Status();
void Log_Write_Sonar();
void Log_Arm_Disarm();
void Log_Write_RC(void);
void Log_Write_Vehicle_Startup_Messages();
void Log_Write_AOA_SSA();
@ -947,9 +946,6 @@ private:
void startup_INS_ground(void);
bool should_log(uint32_t mask);
int8_t throttle_percentage(void);
void change_arm_state(void);
bool disarm_motors(void);
bool arm_motors(AP_Arming::Method method, bool do_arming_checks=true);
bool auto_takeoff_check(void);
void takeoff_calc_roll(void);
void takeoff_calc_pitch(void);
@ -1052,7 +1048,6 @@ private:
void publish_osd_info();
#endif
void accel_cal_update(void);
void update_soft_armed();
#if SOARING_ENABLED == ENABLED
void update_soaring();
#endif

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@ -58,20 +58,6 @@ void RC_Channel_Plane::init_aux_function(const RC_Channel::aux_func_t ch_option,
void RC_Channel_Plane::do_aux_function(const aux_func_t ch_option, const aux_switch_pos_t ch_flag)
{
switch(ch_option) {
case AUX_FUNC::ARMDISARM:
// arm or disarm the vehicle
switch (ch_flag) {
case HIGH:
plane.arm_motors(AP_Arming::Method::AUXSWITCH, true);
break;
case MIDDLE:
// nothing
break;
case LOW:
plane.disarm_motors();
break;
}
break;
case AUX_FUNC::INVERTED:
plane.inverted_flight = (ch_flag == HIGH);
break;

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@ -47,7 +47,7 @@ void AP_AdvancedFailsafe_Plane::terminate_vehicle(void)
plane.quadplane.afs_terminate();
// also disarm to ensure that ignition is cut
plane.disarm_motors();
plane.arming.disarm();
}
void AP_AdvancedFailsafe_Plane::setup_IO_failsafe(void)

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@ -555,7 +555,7 @@ bool Plane::verify_takeoff()
uint32_t now = AP_HAL::millis();
if (now - takeoff_state.start_time_ms > (uint32_t)(1000U * g2.takeoff_timeout)) {
gcs().send_text(MAV_SEVERITY_INFO, "Takeoff timeout at %.1f m/s", ground_speed);
plane.disarm_motors();
plane.arming.disarm();
mission.reset();
}
}

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@ -117,7 +117,6 @@ enum log_messages {
TYPE_GROUNDSTART_MSG,
LOG_RC_MSG,
LOG_SONAR_MSG,
LOG_ARM_DISARM_MSG,
LOG_STATUS_MSG,
LOG_QTUN_MSG,
LOG_PARAMTUNE_MSG,
@ -145,7 +144,7 @@ enum log_messages {
#define MASK_LOG_CAMERA (1<<12)
#define MASK_LOG_RC (1<<13)
#define MASK_LOG_SONAR (1<<14)
#define MASK_LOG_ARM_DISARM (1<<15)
// #define MASK_LOG_ARM_DISARM (1<<15)
#define MASK_LOG_IMU_RAW (1UL<<19)
// altitude control algorithms

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@ -174,7 +174,7 @@ void Plane::handle_battery_failsafe(const char *type_str, const int8_t action)
snprintf(battery_type_str, 17, "%s battery", type_str);
afs.gcs_terminate(true, battery_type_str);
#else
disarm_motors();
arming.disarm();
#endif
break;

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@ -305,7 +305,7 @@ void Plane::crash_detection_update(void)
}
else {
if (aparm.crash_detection_enable & CRASH_DETECT_ACTION_BITMASK_DISARM) {
disarm_motors();
arming.disarm();
}
if (crashed_near_land_waypoint) {
gcs().send_text(MAV_SEVERITY_CRITICAL, "Hard landing detected");

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@ -2543,7 +2543,7 @@ void QuadPlane::check_land_complete(void)
return;
}
if (land_detector(4000)) {
plane.disarm_motors();
plane.arming.disarm();
poscontrol.state = QPOS_LAND_COMPLETE;
gcs().send_text(MAV_SEVERITY_INFO,"Land complete");
// reload target airspeed which could have been modified by the mission

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@ -146,7 +146,7 @@ void Plane::rudder_arm_disarm_check()
}
} else {
//time to arm!
arm_motors(AP_Arming::Method::RUDDER);
arming.arm(AP_Arming::Method::RUDDER);
rudder_arm_timer = 0;
}
} else {
@ -165,7 +165,7 @@ void Plane::rudder_arm_disarm_check()
}
} else {
//time to disarm!
disarm_motors();
arming.disarm();
rudder_arm_timer = 0;
}
} else {

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@ -456,21 +456,18 @@ int8_t Plane::throttle_percentage(void)
}
/*
update AHRS soft arm state and log as needed
*/
void Plane::change_arm_state(void)
update HAL soft arm state and log as needed
*/
void AP_Arming_Plane::change_arm_state(void)
{
Log_Arm_Disarm();
Log_Write_Arm_Disarm();
update_soft_armed();
quadplane.set_armed(hal.util->get_soft_armed());
plane.quadplane.set_armed(hal.util->get_soft_armed());
}
/*
arm motors
*/
bool Plane::arm_motors(const AP_Arming::Method method, const bool do_arming_checks)
bool AP_Arming_Plane::arm(const AP_Arming::Method method, const bool do_arming_checks)
{
if (!arming.arm(method, do_arming_checks)) {
if (!AP_Arming::arm(method, do_arming_checks)) {
return false;
}
@ -481,18 +478,18 @@ bool Plane::arm_motors(const AP_Arming::Method method, const bool do_arming_chec
/*
disarm motors
*/
bool Plane::disarm_motors(void)
bool AP_Arming_Plane::disarm(void)
{
if (!arming.disarm()) {
if (!AP_Arming::disarm()) {
return false;
}
if (control_mode != &mode_auto) {
if (plane.control_mode != &plane.mode_auto) {
// reset the mission on disarm if we are not in auto
mission.reset();
plane.mission.reset();
}
// suppress the throttle in auto-throttle modes
throttle_suppressed = auto_throttle_mode;
plane.throttle_suppressed = plane.auto_throttle_mode;
//only log if disarming was successful
change_arm_state();
@ -502,10 +499,10 @@ bool Plane::disarm_motors(void)
#if QAUTOTUNE_ENABLED
//save qautotune gains if enabled and success
if (control_mode == &mode_qautotune) {
quadplane.qautotune.save_tuning_gains();
if (plane.control_mode == &plane.mode_qautotune) {
plane.quadplane.qautotune.save_tuning_gains();
} else {
quadplane.qautotune.reset();
plane.quadplane.qautotune.reset();
}
#endif