mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-03 15:58:53 +08:00
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>
This commit is contained in:
co-authored by
Ramon Roche
parent
8e6d2ebe4a
commit
88d623bedb
@@ -0,0 +1,47 @@
|
||||
# 测试 MC_01 - 手动模式
|
||||
|
||||
## Objective
|
||||
|
||||
To test that manual flight modes work as expected
|
||||
|
||||
## Preflight
|
||||
|
||||
Ensure that the drone can go into Stabilized, Altitude, Position mode while still on the ground
|
||||
|
||||
## Flight Tests
|
||||
|
||||
❏ 自稳
|
||||
|
||||
❏ Pitch/Roll/Yaw response 1:1
|
||||
|
||||
❏ Throttle response 1:1
|
||||
|
||||
❏ 高度
|
||||
|
||||
❏ Vertical position should hold current value with stick centered
|
||||
|
||||
❏ Pitch/Roll/Yaw response 1:1
|
||||
|
||||
❏ Throttle response set to Climbs/Descend rate
|
||||
|
||||
❏ 定点
|
||||
|
||||
❏ Horizontal position should hold current value with stick centered
|
||||
|
||||
❏ Vertical position should hold current value with stick centered
|
||||
|
||||
❏ Throttle response set to Climbs/Descend rate
|
||||
|
||||
❏ Pitch/Roll/Yaw response set to Pitch/Roll/Yaw rates
|
||||
|
||||
❏ Landing
|
||||
|
||||
❏ Land in Position mode with the throttle below 40%
|
||||
|
||||
❏ 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))
|
||||
|
||||
## 预期成果
|
||||
|
||||
- 当油门升高时,起飞应该是平稳的
|
||||
- 在上述任何飞行模式中都不应出现振荡
|
||||
- 着陆时,直升机不应在地面上反弹
|
||||
Reference in New Issue
Block a user