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FW Position Control: improve/shorten param descriptions 

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
This commit is contained in:
Silvan Fuhrer 2023-09-28 14:22:37 +02:00
parent 8bc3785345
commit 913a7ea295
1 changed files with 8 additions and 17 deletions
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25
src/modules/fw_pos_control/fw_path_navigation_params.c
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@ -1,6 +1,6 @@
/****************************************************************************
*
* Copyright (c) 2013-2016 PX4 Development Team. All rights reserved.
* Copyright (c) 2013-2023 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
@ -249,9 +249,8 @@ PARAM_DEFINE_FLOAT(FW_R_LIM, 50.0f);
/**
* Throttle limit max
*
* This is the maximum throttle % that can be used by the controller.
* For overpowered aircraft, this should be reduced to a value that
* provides sufficient thrust to climb at the maximum pitch angle PTCH_MAX.
* Maximum throttle limit in altitude controlled modes.
* Should be set accordingly to achieve FW_T_CLMB_MAX.
*
* @unit norm
* @min 0.0
@ -265,11 +264,9 @@ PARAM_DEFINE_FLOAT(FW_THR_MAX, 1.0f);
/**
* Throttle limit min
*
* This is the minimum throttle % that can be used by the controller.
* For electric aircraft this will normally be set to zero, but can be set
* to a small non-zero value if a folding prop is fitted to prevent the
* prop from folding and unfolding repeatedly in-flight or to provide
* some aerodynamic drag from a turning prop to improve the descent rate.
* Minimum throttle limit in altitude controlled modes.
* Usually set to 0 but can be increased to prevent the motor from stopping when
* descending, which can increase achievable descent rates.
*
* For aircraft with internal combustion engine this parameter should be set
* for desired idle rpm.
@ -382,10 +379,7 @@ PARAM_DEFINE_INT32(FW_LND_USETER, 1);
*
* When disabled, the landing configuration (flaps, landing airspeed, etc.) is only activated
* on the final approach to landing. When enabled, it is already activated when entering the
* final loiter-down (loiter-to-alt) waypoint before the landing approach. This shifts the (often large)
* altitude and airspeed errors caused by the configuration change away from the ground such that
* these are not so critical. It also gives the controller enough time to adapt to the new
* configuration such that the landing approach starts with a cleaner initial state.
* final loiter-down (loiter-to-alt) waypoint before the landing approach.
*
* @boolean
*
@ -989,8 +983,6 @@ PARAM_DEFINE_INT32(FW_LND_ABORT, 3);
* system more robust against disturbances (turbulence) in high wind.
* Only applies to AUTO flight mode.
*
* airspeed_min_adjusted = FW_AIRSPD_MIN + FW_WIND_ARSP_SC * wind.length()
*
* @min 0
* @decimal 2
* @increment 0.01
@ -999,10 +991,9 @@ PARAM_DEFINE_INT32(FW_LND_ABORT, 3);
PARAM_DEFINE_FLOAT(FW_WIND_ARSP_SC, 0.f);
/**
* FW Launch detection
* Fixed-wing launch detection
*
* Enables automatic launch detection based on measured acceleration. Use for hand- or catapult-launched vehicles.
* Only available for fixed-wing vehicles.
* Not compatible with runway takeoff.
*
* @boolean