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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-11-11 06:11:37 +08:00
commander: use new failsafe state machine and add user intention class
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@@ -283,13 +283,14 @@ PARAM_DEFINE_INT32(COM_ARM_SWISBTN, 0);
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PARAM_DEFINE_INT32(COM_LOW_BAT_ACT, 0);
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/**
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* Delay between battery state change and failsafe reaction
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* Delay between failsafe condition triggered and failsafe reaction
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*
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* Battery state requires action -> wait COM_BAT_ACT_T seconds in Hold mode
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* for the user to realize and take a custom action
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* -> React with failsafe action COM_LOW_BAT_ACT
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* Before entering failsafe (RTL, Land, Hold), wait COM_FAIL_ACT_T seconds in Hold mode
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* for the user to realize.
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* During that time the user cannot take over control.
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* Afterwards the configured failsafe action is triggered and the user may take over.
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*
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* A zero value disables the delay.
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* A zero value disables the delay and the user cannot take over via stick movements (switching modes is still allowed).
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*
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* @group Commander
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* @unit s
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@@ -297,7 +298,7 @@ PARAM_DEFINE_INT32(COM_LOW_BAT_ACT, 0);
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* @max 25.0
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* @decimal 3
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*/
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PARAM_DEFINE_FLOAT(COM_BAT_ACT_T, 5.f);
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PARAM_DEFINE_FLOAT(COM_FAIL_ACT_T, 5.f);
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/**
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* Imbalanced propeller failsafe mode
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@@ -319,7 +320,7 @@ PARAM_DEFINE_INT32(COM_IMB_PROP_ACT, 0);
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/**
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* Time-out to wait when offboard connection is lost before triggering offboard lost action.
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*
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* See COM_OBL_ACT and COM_OBL_RC_ACT to configure action.
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* See COM_OBL_RC_ACT to configure action.
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*
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* @group Commander
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* @unit s
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@@ -329,27 +330,10 @@ PARAM_DEFINE_INT32(COM_IMB_PROP_ACT, 0);
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*/
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PARAM_DEFINE_FLOAT(COM_OF_LOSS_T, 1.0f);
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/**
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* Set offboard loss failsafe mode
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*
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* The offboard loss failsafe will only be entered after a timeout,
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* set by COM_OF_LOSS_T in seconds.
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*
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* @value -1 Disabled
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* @value 0 Land mode
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* @value 1 Hold mode
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* @value 2 Return mode
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* @value 3 Terminate
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* @value 4 Lockdown
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*
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* @group Commander
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*/
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PARAM_DEFINE_INT32(COM_OBL_ACT, 0);
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/**
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* Set command after a quadchute
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*
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* @value -1 No action: stay in current flight mode
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* @value -1 Warning only
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* @value 0 Return mode
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* @value 1 Land mode
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* @value 2 Hold mode
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@@ -358,12 +342,11 @@ PARAM_DEFINE_INT32(COM_OBL_ACT, 0);
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PARAM_DEFINE_INT32(COM_QC_ACT, 0);
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/**
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* Set offboard loss failsafe mode when RC is available
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* Set offboard loss failsafe mode
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*
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* The offboard loss failsafe will only be entered after a timeout,
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* set by COM_OF_LOSS_T in seconds.
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*
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* @value -1 Disabled
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* @value 0 Position mode
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* @value 1 Altitude mode
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* @value 2 Manual
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@@ -371,7 +354,7 @@ PARAM_DEFINE_INT32(COM_QC_ACT, 0);
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* @value 4 Land mode
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* @value 5 Hold mode
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* @value 6 Terminate
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* @value 7 Lockdown
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* @value 7 Disarm
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* @group Commander
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*/
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PARAM_DEFINE_INT32(COM_OBL_RC_ACT, 0);
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@@ -676,10 +659,10 @@ PARAM_DEFINE_INT32(COM_ARM_MIS_REQ, 0);
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*
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* If Altitude/Manual is selected: assume use of remote control after fallback. Switch to Altitude mode if a height estimate is available, else switch to MANUAL.
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*
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* If Land/Terminate is selected: assume no use of remote control after fallback. Switch to Land mode if a height estimate is available, else switch to TERMINATION.
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* If Land/Descend is selected: assume no use of remote control after fallback. Switch to Land mode if a height estimate is available, else switch to Descend.
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*
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* @value 0 Altitude/Manual
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* @value 1 Land/Terminate
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* @value 1 Land/Descend
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*
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* @group Commander
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*/
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@@ -813,7 +796,7 @@ PARAM_DEFINE_INT32(COM_TAKEOFF_ACT, 0);
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* @value 2 Return mode
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* @value 3 Land mode
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* @value 5 Terminate
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* @value 6 Lockdown
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* @value 6 Disarm
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* @min 0
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* @max 6
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*
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@@ -832,7 +815,7 @@ PARAM_DEFINE_INT32(NAV_DLL_ACT, 0);
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* @value 2 Return mode
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* @value 3 Land mode
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* @value 5 Terminate
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* @value 6 Lockdown
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* @value 6 Disarm
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* @min 1
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* @max 6
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*
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@@ -862,7 +845,7 @@ PARAM_DEFINE_INT32(COM_RCL_EXCEPT, 0);
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*
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* @min 0
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* @max 3
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* @value 0 Disabled
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* @value 0 Warning only
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* @value 1 Hold mode
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* @value 2 Land mode
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* @value 3 Return mode
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@@ -988,8 +971,8 @@ PARAM_DEFINE_INT32(COM_POWER_COUNT, 1);
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/**
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* Timeout for detecting a failure after takeoff
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*
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* A non-zero, positive value specifies the timeframe in seconds within failure detector is allowed to put the vehicle into
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* a lockdown state if attitude exceeds the limits defined in FD_FAIL_P and FD_FAIL_R.
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* A non-zero, positive value specifies the timeframe in seconds within failure detector is allowed to disarm the vehicle
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* if attitude exceeds the limits defined in FD_FAIL_P and FD_FAIL_R.
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* The check is not executed for flight modes that do support acrobatic maneuvers, e.g: Acro (MC/FW) and Manual (FW).
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* A zero or negative value means that the check is disabled.
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*
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