mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-22 07:43:37 +08:00
97 lines
2.7 KiB
C
97 lines
2.7 KiB
C
/****************************************************************************
|
|
*
|
|
* 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);
|