mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-07-16 06:40:34 +08:00
Daniel Agar
102 lines
2.9 KiB
C
102 lines
2.9 KiB
C
/****************************************************************************
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*
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* Copyright (c) 2014 PX4 Development Team. All rights reserved.
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*
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* Redistribution and use in source and binary forms, with or without
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* modification, are permitted provided that the following conditions
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* are met:
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*
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* 1. Redistributions of source code must retain the above copyright
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* notice, this list of conditions and the following disclaimer.
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* 2. Redistributions in binary form must reproduce the above copyright
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* notice, this list of conditions and the following disclaimer in
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* the documentation and/or other materials provided with the
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* distribution.
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* 3. Neither the name PX4 nor the names of its contributors may be
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* used to endorse or promote products derived from this software
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* without specific prior written permission.
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*
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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* AS IS AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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* POSSIBILITY OF SUCH DAMAGE.
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*
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****************************************************************************/
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/**
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* @file gpsfailure_params.c
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*
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* Parameters for GPSF navigation mode
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*
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* @author Thomas Gubler <thomasgubler@gmail.com>
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*/
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/*
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* GPS Failure Navigation Mode parameters, accessible via MAVLink
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*/
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/**
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* Loiter time
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*
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* The amount of time in seconds the system should do open loop loiter and wait for gps recovery
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* before it goes into flight termination.
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*
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* @unit s
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* @min 0.0
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* @max 3600.0
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* @decimal 0
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* @increment 1
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* @group GPS Failure Navigation
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*/
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PARAM_DEFINE_FLOAT(NAV_GPSF_LT, 30.0f);
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/**
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* Open loop loiter roll
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*
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* Roll in degrees during the open loop loiter
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*
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* @unit deg
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* @min 0.0
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* @max 30.0
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* @decimal 1
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* @increment 0.5
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* @group GPS Failure Navigation
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*/
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PARAM_DEFINE_FLOAT(NAV_GPSF_R, 15.0f);
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/**
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* Open loop loiter pitch
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*
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* Pitch in degrees during the open loop loiter
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*
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* @unit deg
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* @min -30.0
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* @max 30.0
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* @decimal 1
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* @increment 0.5
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* @group GPS Failure Navigation
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*/
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PARAM_DEFINE_FLOAT(NAV_GPSF_P, 0.0f);
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/**
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* Open loop loiter thrust
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*
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* Thrust value which is set during the open loop loiter
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*
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* @unit norm
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* @min 0.0
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* @max 1.0
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* @decimal 2
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* @increment 0.05
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* @group GPS Failure Navigation
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*/
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PARAM_DEFINE_FLOAT(NAV_GPSF_TR, 0.7f);
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