> For the complete documentation index, see [llms.txt](https://px4.gitbook.io/px4-user-guide/llms.txt). Markdown versions of documentation pages are available by appending `.md` to page URLs; this page is available as [Markdown](https://px4.gitbook.io/px4-user-guide/development/test_and_ci/test_flights/mc_01_manual_modes.md).

# Test MC\_01 - Manual Modes

## Arm and Take-off

❏ Set flight mode to stabilize and Arm

❏ Take-off by raising the throttle

## Flight

❏ Stabilized

&#x20;   ❏ Pitch/Roll/Yaw response 1:1

&#x20;   ❏ Throttle response 1:1

❏ Altitude

&#x20;   ❏ Vertical position should hold current value with stick centered

&#x20;   ❏ Pitch/Roll/Yaw response 1:1

&#x20;   ❏ Throttle response set to Climbs/Descend rate

❏ Position

&#x20;   ❏ Horizontal position should hold current value with stick centered

&#x20;   ❏ Vertical position should hold current value with stick centered

&#x20;   ❏ Throttle response set to Climbs/Descend rate

&#x20;   ❏ 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](/px4-user-guide/advanced_config/parameter_reference.md#COM_DISARM_LAND))

## Expected Results

* Take-off should be smooth as throttle is raised
* No oscillations should present in any of the above flight modes
* Upon landing, copter should not bounce on the ground
