gpsfailure_params.c
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/****************************************************************************
*
* Copyright (c) 2014 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
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* AS IS AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/**
* @file gpsfailure_params.c
*
* Parameters for GPSF navigation mode
*
*/
/**
* Loiter time
*
* The time in seconds the system should do open loop loiter and wait for GPS recovery
* before it goes into flight termination. Set to 0 to disable.
*
* @unit s
* @min 0.0
* @max 3600.0
* @decimal 0
* @increment 1
* @group GPS Failure Navigation
*/
PARAM_DEFINE_FLOAT(NAV_GPSF_LT, 0.0f);
/**
* Fixed bank angle
*
* Roll in degrees during the loiter
*
* @unit deg
* @min 0.0
* @max 30.0
* @decimal 1
* @increment 0.5
* @group GPS Failure Navigation
*/
PARAM_DEFINE_FLOAT(NAV_GPSF_R, 15.0f);
/**
* Fixed pitch angle
*
* Pitch in degrees during the open loop loiter
*
* @unit deg
* @min -30.0
* @max 30.0
* @decimal 1
* @increment 0.5
* @group GPS Failure Navigation
*/
PARAM_DEFINE_FLOAT(NAV_GPSF_P, 0.0f);
/**
* Thrust
*
* Thrust value which is set during the open loop loiter
*
* @unit norm
* @min 0.0
* @max 1.0
* @decimal 2
* @increment 0.05
* @group GPS Failure Navigation
*/
PARAM_DEFINE_FLOAT(NAV_GPSF_TR, 0.0f);