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* Add vitepress tree * Update existing workflows so they dont trigger on changes in the docs path * Add nojekyll, package.json, LICENCE etc * Add crowdin docs upload/download scripts * Add docs flaw checker workflows * Used docs prefix for docs workflows * Crowdin obvious fixes * ci: docs move to self hosted runner runs on a beefy server for faster builds Signed-off-by: Ramon Roche <mrpollo@gmail.com> * ci: don't run build action for docs or ci changes Signed-off-by: Ramon Roche <mrpollo@gmail.com> * ci: update runners Signed-off-by: Ramon Roche <mrpollo@gmail.com> * Add docs/en * Add docs assets and scripts * Fix up editlinks to point to PX4 sources * Download just the translations that are supported * Add translation sources for zh, uk, ko * Update latest tranlsation and uorb graphs * update vitepress to latest --------- Signed-off-by: Ramon Roche <mrpollo@gmail.com> Co-authored-by: Ramon Roche <mrpollo@gmail.com>
79 lines
4.4 KiB
Markdown
79 lines
4.4 KiB
Markdown
# 비행 중단 설정
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The _Flight termination_ [failsafe action](../config/safety.md#failsafe-actions) may be triggered by a [safety check](../config/safety.md) (e.g. RC Loss, geofence violation, etc. on any vehicle type or in any flight mode), or by the [Failure Detector](../config/safety.md#failure-detector).
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:::info
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Flight termination may also be triggered from a ground station or companion computer using the MAVLink [MAV_CMD_DO_FLIGHTTERMINATION](https://mavlink.io/en/messages/common.html#MAV_CMD_DO_FLIGHTTERMINATION) command.
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This is sent, for example, when you call the [MAVSDK Action plugin](https://mavsdk.mavlink.io/main/en/cpp/api_reference/classmavsdk_1_1_action.html#classmavsdk_1_1_action_1a47536c4a4bc8367ccd30a92eb09781c5) `terminate()` or `terminate_async()` methods.
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:::
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When _Flight termination_ is activated, PX4 simultaneously turns off all controllers and sets all PWM outputs to their failsafe values.
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Depending on what devices are connected, the PWM failsafe outputs can be used to:
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- Deploy a [parachute](../peripherals/parachute.md).
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- 랜딩기어 펼치기.
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- 카메라를 보호하기 위해 PWM방식으로 연결된 짐벌을 안전 각도(또는 수납 위치) 로 움직이기.
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- 에어백 같은 팽창 장비 가동하기.
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- 알람 울리기.
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:::tip
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PX4는 어떤 안전 장치가 장착되어 있는지 알지 못합니다. 미리 정의된 PWM 값 세트를 출력에 적용하기만 하면 됩니다.
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After triggering you should unplug the battery as soon as possible.
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You will need to reboot/power cycle the vehicle before it can be used again.
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:::tip
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PX4 does not know what safety devices are attached - it just applies a predefined set of PWM values to its outputs.
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:::
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:::tip
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Failsafe values are applied to all outputs on termination.
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전원이 끊기거나 자동조종장치가 완전히 충돌하면 안전 장치가 작동하지 않습니다.
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:::
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:::info
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This is _not_ an independent _Flight Termination System_.
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If power is lost or if the autopilot crashes completely, the failsafe devices will not be triggered.
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:::
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## 하드웨어 설정
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Any _safety device(s)_ (e.g. a [parachute](../peripherals/parachute.md)) that can be triggered by changing a PWM value can be used, and may be connected to any free PWM port (both MAIN and AUX).
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:::info
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If you're using Pixhawk-series board you will have to separately power the servo rail (i.e. from a 5V BEC, which is often also available from your ESC).
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:::
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## 소프트웨어 설정
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The [Safety](../config/safety.md) topic explains how to set the _flight termination_ as the [failsafe action](../config/safety.md#failsafe-actions) to be performed for particular failsafe check.
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The [Failure Detector](../config/safety.md#failure-detector) can also (optionally) be configured to trigger flight termination if the vehicle flips (exceeds a certain attitude) or if failure is detected by an external automatic trigger system (ATS):
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- Enable the failure detector during flight by setting [CBRK_FLIGHTTERM=0](../advanced_config/parameter_reference.md#CBRK_FLIGHTTERM).
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- [Safety > Failure Detector > Attitude Trigger](../config/safety.md#attitude-trigger) explains how to configure the attitude limits that trigger _Flight termination_.
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::: info
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During _takeoff_ excessive attitutes will trigger _lockdown_ (kill motors, but not launch parachute) rather than flight termination.
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This is always enabled, irrespective of the value of `CBRK_FLIGHTTERM`.
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:::
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- [Safety > External Automatic Trigger System (ATS)](../config/safety.md#external-automatic-trigger-system-ats) explains how to configure an external trigger system.
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아래의 다이어그램은 비행 중단과 관련된 논리적 흐름을 보여 줍니다.
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- [PWM_MAIN_DISn](../advanced_config/parameter_reference.md#PWM_MAIN_DIS1) to the device's "OFF" PWM value.
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- [PWM_MAIN_FAILn](../advanced_config/parameter_reference.md#PWM_MAIN_FAIL1) to the device's "ON" PWM value.
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마지막으로, 모든 모터에 대해 <code>PWM_AUX_FAILn</code> 및 <code>PWM_MAIN_FAILn</code> PWM 값을 설정합니다.
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- [PWM_AUX_DIS1](../advanced_config/parameter_reference.md#PWM_AUX_DIS1) to the device's "OFF" PWM value.
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- [PWM_AUX_FAILn](../advanced_config/parameter_reference.md#PWM_AUX_FAIL1) to the device's "ON" PWM value.
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Finally, set the `PWM_AUX_FAILn` and `PWM_MAIN_FAILn` PWM values for any motors.
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## 로직 다이어그램
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The diagram below shows the logical flow around flight termination.
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