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fw-autotune: update docs
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@ -98,8 +98,7 @@ The test steps are:
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</div><div v-else-if="$frontmatter.frame === 'Plane'">
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4. The drone will first start to perform quick roll motions followed by pitch and yaw motions. When [`FW_AT_SYSID_TYPE`](../advanced_config/parameter_reference.md#FW_AT_SYSID_TYPE) is set to linear/logarithmic sine sweep (recommended), the max rates are approximately 45 deg/s for roll and 30 deg/s for pitch and yaw.
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The progress is shown in the progress bar, next to the _Autotune_ button.
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4. The drone will first start to perform quick roll motions followed by pitch and yaw motions. When [`FW_AT_SYSID_TYPE`](../advanced_config/parameter_reference.md#FW_AT_SYSID_TYPE) is set to linear/logarithmic sine sweep (recommended), the max rates reached during the maneuvers are 75% of the maximum configured roll (`FW_R_RMAX`), pitch (`FW_P_RMAX_NEG`, `FW_P_RMAX_POS`) and yaw (`FW_Y_RMAX`) rates. The progress is shown in the progress bar, next to the _Autotune_ button.
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</div>
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<div style="display: inline;" v-if="$frontmatter.frame === 'Multicopter'">
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@ -194,7 +193,7 @@ Increase the [MC_AT_SYSID_AMP](../advanced_config/parameter_reference.md#MC_AT_S
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</div>
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<div v-else-if="$frontmatter.frame === 'Plane'">
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By default, the autotune maneuvers ensure that a sufficient angular rate is reached for system identification. The target rates are approximately 45 deg/s for roll and 30 deg/s for pitch and yaw.
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By default, the autotune maneuvers ensure that a sufficient angular rate is reached for system identification, corresponding to 75% of the configured maximum roll (`FW_R_RMAX`), pitch (`FW_P_RMAX_NEG`, `FW_P_RMAX_POS`) and yaw (`FW_Y_RMAX`) rates.
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If the signal-to-noise ratio of the vehicle is low, the system identification algorithm might have issues finding the correct coefficients. Ensure that there is no excessive noise and/or platform vibration.
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