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* updated test cards for optical flow flights * Update docs/en/test_cards/mc_07_optical_flow_failure.md Co-authored-by: Jacob Dahl <37091262+dakejahl@users.noreply.github.com> * updated docs * fixed mis-type in url * subedit * Update docs/en/test_cards/mc_06_optical_flow.md Co-authored-by: Hamish Willee <hamishwillee@gmail.com> * updated test card * changes to file name and some instructions --------- Co-authored-by: Jacob Dahl <37091262+dakejahl@users.noreply.github.com> Co-authored-by: Hamish Willee <hamishwillee@gmail.com>
47 lines
1.6 KiB
Markdown
47 lines
1.6 KiB
Markdown
# 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 mode](../flight_modes_mc/manual_stabilized.md)
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❏ Takeoff in stabilized 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 mode](../flight_modes_mc/position.md)
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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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## Landing
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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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## Expected Results
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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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