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https://github.com/ArduPilot/ardupilot
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Copter: rename variables used for NAV_DELAY command
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@ -380,8 +380,8 @@ private:
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uint32_t brake_timeout_ms;
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// Delay the next navigation command
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int32_t delay_time_max; // used for delaying the navigation commands (eg land,takeoff etc.)
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uint32_t delay_time_start;
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int32_t nav_delay_time_max; // used for delaying the navigation commands (eg land,takeoff etc.)
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uint32_t nav_delay_time_start;
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// Flip
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Vector3f flip_orig_attitude; // original copter attitude before flip
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@ -524,16 +524,16 @@ void Copter::do_nav_guided_enable(const AP_Mission::Mission_Command& cmd)
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// do_nav_delay - Delay the next navigation command
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void Copter::do_nav_delay(const AP_Mission::Mission_Command& cmd)
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{
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delay_time_start = millis();
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nav_delay_time_start = millis();
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if (cmd.content.nav_delay.seconds > 0) {
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// relative delay
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delay_time_max = cmd.content.nav_delay.seconds * 1000; // convert seconds to milliseconds
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nav_delay_time_max = cmd.content.nav_delay.seconds * 1000; // convert seconds to milliseconds
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} else {
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// absolute delay to utc time
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delay_time_max = hal.util->get_time_utc(cmd.content.nav_delay.hour_utc, cmd.content.nav_delay.min_utc, cmd.content.nav_delay.sec_utc, 0);
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nav_delay_time_max = hal.util->get_time_utc(cmd.content.nav_delay.hour_utc, cmd.content.nav_delay.min_utc, cmd.content.nav_delay.sec_utc, 0);
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}
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gcs_send_text_fmt(MAV_SEVERITY_INFO, "Delaying %u sec",(unsigned int)(delay_time_max/1000));
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gcs_send_text_fmt(MAV_SEVERITY_INFO, "Delaying %u sec",(unsigned int)(nav_delay_time_max/1000));
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}
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#if PARACHUTE == ENABLED
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@ -762,8 +762,8 @@ bool Copter::verify_nav_guided_enable(const AP_Mission::Mission_Command& cmd)
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// verify_nav_delay - check if we have waited long enough
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bool Copter::verify_nav_delay(const AP_Mission::Mission_Command& cmd)
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{
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if (millis() - delay_time_start > (uint32_t)MAX(delay_time_max,0)) {
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delay_time_max = 0;
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if (millis() - nav_delay_time_start > (uint32_t)MAX(nav_delay_time_max,0)) {
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nav_delay_time_max = 0;
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return true;
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}
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return false;
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