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@ -641,7 +641,7 @@ PARAM_DEFINE_INT32(COM_ARM_AUTH, 256010); |
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/**
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/**
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* Loss of position failsafe activation delay. |
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* Loss of position failsafe activation delay. |
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* |
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* |
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* This sets number of second that the position checks need to be failed before the failsafe will activate. |
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* This sets number of seconds that the position checks need to be failed before the failsafe will activate. |
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* The default value has been optimised for rotary wing applications. For fixed wing applications, a larger value between 5 and 10 should be used. |
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* The default value has been optimised for rotary wing applications. For fixed wing applications, a larger value between 5 and 10 should be used. |
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* |
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* |
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* @unit sec |
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* @unit sec |
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@ -653,7 +653,7 @@ PARAM_DEFINE_INT32(COM_POS_FS_DELAY, 1); |
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/**
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/**
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* Loss of position probation delay at takeoff. |
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* Loss of position probation delay at takeoff. |
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* |
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* |
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* The probation delay is number of seconds that the EKF innovation checks need to pass for the positon to be declared good after it has been declared bad. |
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* The probation delay is the number of seconds that the EKF innovation checks need to pass for the position to be declared good after it has been declared bad. |
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* The probation delay will be reset to this parameter value when takeoff is detected. |
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* The probation delay will be reset to this parameter value when takeoff is detected. |
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* After takeoff, if position checks are passing, the probation delay will reduce by one second for every lapsed second of valid position down to a minimum of 1 second. |
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* After takeoff, if position checks are passing, the probation delay will reduce by one second for every lapsed second of valid position down to a minimum of 1 second. |
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* If position checks are failing, the probation delay will increase by COM_POS_FS_GAIN seconds for every lapsed second up to a maximum of 100 seconds. |
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* If position checks are failing, the probation delay will increase by COM_POS_FS_GAIN seconds for every lapsed second up to a maximum of 100 seconds. |
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