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https://github.com/ArduPilot/ardupilot
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AP_Logger: Updates to log message units and help text
Link LGR.WOW to AP_LandingGear::LG_WOW_State enum Set quaternion component units to no-unit from UNKNOWN Separate descriptions for PID and PIQ messages Co-authored-by: Peter Hall <33176108+IamPete1@users.noreply.github.com>
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@ -817,7 +817,8 @@ struct PACKED log_VER {
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// @Field: TimeUS: Time since system startup
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// @Field: TimeUS: Time since system startup
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// @Field: LandingGear: Current landing gear state
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// @Field: LandingGear: Current landing gear state
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// @FieldValueEnum: LandingGear: AP_LandingGear::LG_LandingGear_State
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// @FieldValueEnum: LandingGear: AP_LandingGear::LG_LandingGear_State
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// @Field: WeightOnWheels: True if there is weight on wheels
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// @Field: WeightOnWheels: Weight on wheels state
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// @FieldValueEnum: WeightOnWheels: AP_LandingGear::LG_WOW_State
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// @LoggerMessage: MAG
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// @LoggerMessage: MAG
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// @Description: Information received from compasses
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// @Description: Information received from compasses
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@ -901,8 +902,20 @@ struct PACKED log_VER {
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// @Field: Value: parameter value
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// @Field: Value: parameter value
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// @Field: Default: default parameter value for this board and config
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// @Field: Default: default parameter value for this board and config
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// @LoggerMessage: PIDR,PIDP,PIDY,PIDA,PIDS,PIDN,PIDE
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// @LoggerMessage: PIDR
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// @Description: Proportional/Integral/Derivative gain values for Roll/Pitch/Yaw/Altitude/Steering
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// @Description: Proportional/Integral/Derivative gain values for Roll rate
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// @LoggerMessage: PIDP
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// @Description: Proportional/Integral/Derivative gain values for Pitch rate
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// @LoggerMessage: PIDY
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// @Description: Proportional/Integral/Derivative gain values for Yaw rate
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// @LoggerMessage: PIDA
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// @Description: Proportional/Integral/Derivative gain values for vertical acceleration
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// @LoggerMessage: PIDS
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// @Description: Proportional/Integral/Derivative gain values for ground steering yaw rate
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// @LoggerMessage: PIDN
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// @Description: Proportional/Integral/Derivative gain values for North/South velocity
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// @LoggerMessage: PIDE
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// @Description: Proportional/Integral/Derivative gain values for East/West velocity
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// @Field: TimeUS: Time since system startup
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// @Field: TimeUS: Time since system startup
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// @Field: Tar: desired value
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// @Field: Tar: desired value
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// @Field: Act: achieved value
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// @Field: Act: achieved value
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@ -1257,7 +1270,7 @@ LOG_STRUCTURE_FROM_MOUNT \
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"SRTL", "QBHHBfff", "TimeUS,Active,NumPts,MaxPts,Action,N,E,D", "s----mmm", "F----000" }, \
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"SRTL", "QBHHBfff", "TimeUS,Active,NumPts,MaxPts,Action,N,E,D", "s----mmm", "F----000" }, \
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LOG_STRUCTURE_FROM_AVOIDANCE \
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LOG_STRUCTURE_FROM_AVOIDANCE \
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{ LOG_SIMSTATE_MSG, sizeof(log_AHRS), \
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{ LOG_SIMSTATE_MSG, sizeof(log_AHRS), \
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"SIM","QccCfLLffff","TimeUS,Roll,Pitch,Yaw,Alt,Lat,Lng,Q1,Q2,Q3,Q4", "sddhmDU????", "FBBB0GG????", true }, \
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"SIM","QccCfLLffff","TimeUS,Roll,Pitch,Yaw,Alt,Lat,Lng,Q1,Q2,Q3,Q4", "sddhmDU----", "FBBB0GG0000", true }, \
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{ LOG_TERRAIN_MSG, sizeof(log_TERRAIN), \
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{ LOG_TERRAIN_MSG, sizeof(log_TERRAIN), \
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"TERR","QBLLHffHHf","TimeUS,Status,Lat,Lng,Spacing,TerrH,CHeight,Pending,Loaded,ROfs", "s-DU-mm--m", "F-GG-00--0", true }, \
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"TERR","QBLLHffHHf","TimeUS,Status,Lat,Lng,Spacing,TerrH,CHeight,Pending,Loaded,ROfs", "s-DU-mm--m", "F-GG-00--0", true }, \
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LOG_STRUCTURE_FROM_ESC_TELEM \
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LOG_STRUCTURE_FROM_ESC_TELEM \
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