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Move PX4 Guide source into /docs (#24490)
* 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>
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# 测试 MC_01 - 手动模式
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## Objective
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To test that manual flight modes work as expected
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## Preflight
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Ensure that the drone can go into Stabilized, Altitude, Position mode while still on the ground
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## Flight Tests
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❏ 自稳
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❏ Pitch/Roll/Yaw response 1:1
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❏ Throttle response 1:1
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❏ 高度
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❏ Vertical position should hold current value with stick centered
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❏ Pitch/Roll/Yaw response 1:1
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❏ Throttle response set to Climbs/Descend rate
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❏ 定点
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❏ Horizontal position should hold current value with stick centered
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❏ Vertical position should hold current value with stick centered
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❏ Throttle response set to Climbs/Descend rate
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❏ Pitch/Roll/Yaw response set to Pitch/Roll/Yaw rates
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❏ Landing
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❏ Land in Position mode with the throttle below 40%
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❏ Upon touching ground, copter should disarm automatically within 2 seconds (disarm time set by parameter: [COM_DISARM_LAND](../advanced_config/parameter_reference.md#COM_DISARM_LAND))
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## 预期成果
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- 当油门升高时,起飞应该是平稳的
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- 在上述任何飞行模式中都不应出现振荡
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- 着陆时,直升机不应在地面上反弹
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# 测试 MC_02-完全自主
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## Objective
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To test the auto modes such as Mission, RTL, etc...
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## Preflight
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Plan a mission on the ground. Ensure the mission has
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- Takeoff as first waypoint
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- Changes in Altitude throughout the mission
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- Last waypoint is an RTL
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- Duration of 5 to 6 minutes
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## Flight Tests
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❏ Mission
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❏ Auto take-off
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❏ Changes in Altitude throughout the mission
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❏ First waypoint set to Takeoff
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❏ Enable Mission End RTL
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❏ Duration of 5 to 6 minutes
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❏ Auto Disarm on land
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❏ Mission + Manual arm
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❏ Arm in any manual mode
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❏ Engage Auto (Mission Mode) to trigger take-off
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❏ Observe tracking, cornering and proper RTL performance
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❏ Upon touching ground, copter should disarm automatically within 2 seconds (disarm time set by parameter: [COM_DISARM_LAND](../advanced_config/parameter_reference.md#COM_DISARM_LAND))
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❏ RTL
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❏ Arm and takeoff in position mode
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❏ Fly out ~10m from start point
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❏ Engage RTL Mode
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❏ Observe tracking, cornering and proper RTL performance
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## 预期成果
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- 当油门升高时,起飞应该是平稳的
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- 任务应该在第一次尝试时上传
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- 使用 Auto 时飞机应自动起飞
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- Vehicle shoud adjust height to RTL altitude before returning home
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- 着陆时,直升机不应在地面上反弹
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<!--
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MC_002 - Full autonomous
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- Make sure the auto-disarm is enabled
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- QGC open test1_mission.plan and sync to the vehicle
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- Takeoff from QGC start mission slider
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- Check the vehicle completes the mission
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- Let the vehicle to auto land, take manual control if needed and explain the reason in log description.
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- Check the vehicle disarms by itself.
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-->
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# 测试 MC_03 - 自动手动混合
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## Objective
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To test switching between various modes
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## Preflight
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- Takeoff as first waypoint
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- Changes in Altitude throughout the mission
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- Last waypoint is a NOT RTL, but a normal waypoint
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- Duration of 5 to 6 minutes
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## Flight Tests
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❏ Position + Mission
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❏ Arm and take-off in Position mode
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❏ Engage Auto
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❏ Observe tracking and cornering
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❏ Once mission has completed, switch back to Position mode
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❏ Horizontal position should hold current value with stick centered
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❏ Vertical position should hold current value with stick centered
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❏ Throttle response set to Climbs/Descend rate
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❏ Pitch/Roll/Yaw response set to Pitch/Roll/Yaw rates
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❏ Engage RTL
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❏ Upon touching ground, copter should disarm automatically within 2 seconds (disarm time set by parameter: COM_DISARM_LAND)
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❏ Mission + Controller interruption
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❏ Arm and take-off in Position mode
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❏ Engage Auto
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❏ Observe tracking and cornering
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❏ Before the last waypoint mission is reached, move the control sticks and ensure the vehicle goes into Position flight mode
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❏ Manually move the drone over the landing zone
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❏ Engage Land mode
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❏ Upon touching ground, copter should disarm automatically within 2 seconds (disarm time set by parameter: COM_DISARM_LAND)
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## 预期成果
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- 当油门升高时,起飞应该是平稳的
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- 在上述任何飞行模式中都不应出现振荡
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- When moving the control sticks the drone goes into Position flight mode
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- 着陆时,直升机不应在地面上反弹
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# 测试 MC_04 -故障安全测试
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## Objective
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Test RC loss, data link loss, and low battery failsafes.
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## Preflight
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- Verify RC Loss action is Return to Land
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- Verify Data Link Loss action is Return to Land and the timeout is 10 seconds
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- Verify Battery failsafe
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- Action is Return to Land
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- Battery Warn Level is 25%
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- Battery Failsafe Level is 20%
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- Battery Emergency Level is 15%
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## Flight Tests
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❏ RC 损失
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❏ Take off in Altitude mode
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❏ Move at least 20 meters away home position
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❏Turn off RC and check the vehicle returns to home position, wait for the descent and turn on the RC and take over.
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❏ Datalink Loss
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❏ Disconnect telemetry, vehicle should return to home position after 10 seconds, wait for the descent and reconnect the telemetry radio
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❏ Battery Failsafe
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❏ Confirm the warning message is received in QGC
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❏ Confirm the vehicle returns to land on failsafe level
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❏ Confirm the vehicle lands on emergency land level
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# 测试 MC_05-室内飞行(手动模式)
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## 何时使用此测试卡
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- 新建初次飞行
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- 当需要在受限区域复现问题时
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- 可能存在稳定性问题的实验性构建
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- 测试已更换和/或修改的硬件
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## 解锁并起飞
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❏ 设置飞行模式以稳定和布防
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❏ 升高油门起飞
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## 飞行
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❏ 自稳
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❏ Pitch/Roll/Yaw response 1:1
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❏ Throttle response 1:1
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❏ 高度
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❏ Vertical position should hold current value with stick centered
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❏ Pitch/Roll/Yaw response 1:1
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❏ Throttle response set to Climbs/Descend rate
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## 降落
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❏ 以稳定或高度模式着陆,油门低于 40%
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❏ Upon touching ground, copter should disarm automatically within 2 seconds (disarm time set by parameter: [COM_DISARM_LAND](../advanced_config/parameter_reference.md#COM_DISARM_LAND))
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## 预期成果
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- 当油门升高时,起飞应该是平稳的
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- 在上述任何飞行模式中都不应出现振荡
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- 着陆时,直升机不应在地面上反弹
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