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New Crowdin translations - zh-CN (#25483)
Co-authored-by: Crowdin Bot <support+bot@crowdin.com>
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@@ -9,10 +9,10 @@ Test RC loss, data link loss, and low battery failsafes.
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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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- 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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@@ -2,11 +2,19 @@
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## Objective
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To test that optical flow / external vision work as expected
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To test that optical flow works as expected
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## Preflight
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Disconnect all GPS / compasses and ensure vehicle is using optical flow for navigation
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([Setup Information here](../sensor/optical_flow.md))
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Ensure there are no other sources of positioning besides optical flow
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- [EKF2_OF_CTRL](../advanced_config/parameter_reference.md#EKF2_OF_CTRL): `1`
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- [EKF2_GPS_CTRL](../advanced_config/parameter_reference.md#EKF2_GPS_CTRL): `0`
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- [EKF2_EV_CTRL](../advanced_config/parameter_reference.md#EKF2_EV_CTRL): `0`
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- [SYS_HAS_MAG](../advanced_config/parameter_reference.md#SYS_HAS_MAG): `0`
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Ensure that the drone can go into Altitude / Position flight mode while still on the ground
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@@ -39,5 +47,7 @@ Ensure that the drone can go into Altitude / Position flight mode while still on
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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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- Drone should hold altitude in Altitude Flight mode without wandering
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- Drone should hold position within 1 meter in Position Flight mode without pilot moving sticks
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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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@@ -0,0 +1,52 @@
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# Test MC_07 - VIO (Visual-Inertial Odometry)
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## Objective
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To test that external vision (VIO) works as expected
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## Preflight
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Disconnect all GPS / compasses and ensure vehicle is using VIO for navigation
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Ensure that the drone can go into Altitude / Position flight mode while still on the ground
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Ensure there are no other sources of positioning besides VIO:
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- [EKF2_OF_CTRL](../advanced_config/parameter_reference.md#EKF2_OF_CTRL): `0`
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- [EKF2_GPS_CTRL](../advanced_config/parameter_reference.md#EKF2_GPS_CTRL): `0`
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- [EKF2_EV_CTRL](../advanced_config/parameter_reference.md#EKF2_EV_CTRL): `15`
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- [SYS_HAS_MAG](../advanced_config/parameter_reference.md#SYS_HAS_MAG): `0`
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## Flight Tests
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❏ Altitude flight mode
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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 climb/descent rate
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❏ Position flight 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 climb/descent rate
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❏ Pitch/Roll/Yaw response set to pitch/roll/yaw rates
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## 降落
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❏ Land in either Position or Altitude mode with the throttle below 40%
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❏ Upon touching ground, copter should disarm automatically within 2 seconds (default: see [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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- Drone should hold altitude in Altitude Flight mode without wandering
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- Drone should hold position within 1 meter in Position Flight mode without pilot moving sticks
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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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@@ -0,0 +1,46 @@
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# Test MC_08 - DSHOT ESC
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## Objective
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Regression test for DSHOT working with PX4
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## Preflight
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- Ensure vehicle is using a DSHOT ESC.
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- Parameter [DSHOT_BIDIR_EN](../advanced_config/parameter_reference.md#DSHOT_BIDIR_EN) is enabled
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- Parameter [DSHOT_TEL_CFG](../advanced_config/parameter_reference.md#DSHOT_TEL_CFG) is configured (if ESC supports telemetry)
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- Parameter [SDLOG_PROFILE](../advanced_config/parameter_reference.md#SDLOG_PROFILE) has Debug (`5`) checked
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## Flight Tests
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❏ Stabilized Flight mode
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❏ Takeoff in stabilized flight mode to ensure correct motor spin
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❏ Pitch/Roll/Yaw response 1:1
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❏ Throttle response 1:1
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❏ Position flight 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 climb/descent rate
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❏ Pitch/Roll/Yaw response set to pitch/roll/yaw rates
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## 降落
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❏ Land in either Position or Altitude mode with the throttle below 40%
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❏ Upon touching ground, copter should disarm automatically within 2 seconds (default: see [COM_DISARM_LAND](../advanced_config/parameter_reference.md#COM_DISARM_LAND))
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## 预期成果
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- Download flight logs
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- Load into Data Plot Juggler
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- Ensure data is logged for esc_status/esc.0x/esc_rpm
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