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PX4-Autopilot/docs/en/test_cards/mc_07_vio.md
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Andrew WilkinsandHamish Willee 35ff853f76 Docs/test card update (#25451)
* added VIO test card

* added tickets for regression testing

* Subedit

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Co-authored-by: Hamish Willee <hamishwillee@gmail.com>
2025-08-20 12:08:49 +10:00

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# Test MC_07 - VIO (Visual-Inertial Odometry)
## Objective
To test that external vision (VIO) works as expected
## Preflight
Disconnect all GPS / compasses and ensure vehicle is using VIO for navigation
Ensure that the drone can go into Altitude / Position flight mode while still on the ground
Ensure there are no other sources of positioning besides VIO:
- [EKF2_OF_CTRL](../advanced_config/parameter_reference.md#EKF2_OF_CTRL): `0`
- [EKF2_GPS_CTRL](../advanced_config/parameter_reference.md#EKF2_GPS_CTRL): `0`
- [EKF2_EV_CTRL](../advanced_config/parameter_reference.md#EKF2_EV_CTRL): `15`
- [SYS_HAS_MAG](../advanced_config/parameter_reference.md#SYS_HAS_MAG): `0`
## Flight Tests
❏ Altitude flight mode
&nbsp;&nbsp;&nbsp;&nbsp;❏ Vertical position should hold current value with stick centered
&nbsp;&nbsp;&nbsp;&nbsp;❏ Pitch/Roll/Yaw response 1:1
&nbsp;&nbsp;&nbsp;&nbsp;❏ Throttle response set to climb/descent rate
❏ Position flight mode
&nbsp;&nbsp;&nbsp;&nbsp;❏ Horizontal position should hold current value with stick centered
&nbsp;&nbsp;&nbsp;&nbsp;❏ Vertical position should hold current value with stick centered
&nbsp;&nbsp;&nbsp;&nbsp;❏ Throttle response set to climb/descent rate
&nbsp;&nbsp;&nbsp;&nbsp;❏ Pitch/Roll/Yaw response set to pitch/roll/yaw rates
## Landing
❏ Land in either Position or Altitude mode with the throttle below 40%
❏ Upon touching ground, copter should disarm automatically within 2 seconds (default: see [COM_DISARM_LAND](../advanced_config/parameter_reference.md#COM_DISARM_LAND))
## Expected Results
- Take-off should be smooth as throttle is raised
- Drone should hold altitude in Altitude Flight mode without wandering
- Drone should hold position within 1 meter in Position Flight mode without pilot moving sticks
- No oscillations should present in any of the above flight modes
- Upon landing, copter should not bounce on the ground