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LibrePilot/flight/Modules/ManualControl/inc/manualcontrol.h

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Flight/Modules: Corrected code to use tabs find ./flight/OpenPilot/Modules/ \! \( -name '*~' -a -prune \) -type f | xargs -I{} bash -c 'echo {}; dos2unix {}; gnuindent -npro -kr -i8 -ts8 -sob -ss -ncs -cp1 -il0 -hnl -l150 {};' git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1776 ebee16cc-31ac-478f-84a7-5cbb03baadba
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/**
******************************************************************************
* @addtogroup OpenPilotModules OpenPilot Modules
OP-193: Weak leveling variant on rate mode. Slowly will return to level.
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* @{
Flight/Modules: Corrected code to use tabs find ./flight/OpenPilot/Modules/ \! \( -name '*~' -a -prune \) -type f | xargs -I{} bash -c 'echo {}; dos2unix {}; gnuindent -npro -kr -i8 -ts8 -sob -ss -ncs -cp1 -il0 -hnl -l150 {};' git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1776 ebee16cc-31ac-478f-84a7-5cbb03baadba
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* @addtogroup ManualControlModule Manual Control Module
* @{
*
* @file manualcontrol.h
* @author The OpenPilot Team, http://www.openpilot.org Copyright (C) 2010.
* @brief ManualControl module. Handles safety R/C link and flight mode.
*
* @see The GNU Public License (GPL) Version 3
*
*****************************************************************************/
/*
* This program is free software; you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation; either version 3 of the License, or
* (at your option) any later version.
*
* This program is distributed in the hope that it will be useful, but
* WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY
* or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
* for more details.
*
* You should have received a copy of the GNU General Public License along
* with this program; if not, write to the Free Software Foundation, Inc.,
* 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA
*/
#ifndef MANUALCONTROL_H
#define MANUALCONTROL_H
OP-329: Enumerate more possible flight modes now like multiple stabilization modes so that the FlightMode field is complete in terms of being informative enough git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2935 ebee16cc-31ac-478f-84a7-5cbb03baadba
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#include "manualcontrolcommand.h"
typedef enum {FLIGHTMODE_UNDEFINED = 0, FLIGHTMODE_MANUAL = 1, FLIGHTMODE_STABILIZED = 2, FLIGHTMODE_GUIDANCE = 3} flightmode_path;
#define PARSE_FLIGHT_MODE(x) ( \
OP-475: Starting to use the new FlightStatus object
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(x == FLIGHTSTATUS_FLIGHTMODE_MANUAL) ? FLIGHTMODE_MANUAL : \
(x == FLIGHTSTATUS_FLIGHTMODE_STABILIZED1) ? FLIGHTMODE_STABILIZED : \
(x == FLIGHTSTATUS_FLIGHTMODE_STABILIZED2) ? FLIGHTMODE_STABILIZED : \
(x == FLIGHTSTATUS_FLIGHTMODE_STABILIZED3) ? FLIGHTMODE_STABILIZED : \
INS: First pass at altitude hold code
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(x == FLIGHTSTATUS_FLIGHTMODE_ALTITUDEHOLD) ? FLIGHTMODE_GUIDANCE : \
OP-475: Starting to use the new FlightStatus object
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(x == FLIGHTSTATUS_FLIGHTMODE_VELOCITYCONTROL) ? FLIGHTMODE_GUIDANCE : \
Create stub for waypoint navigation
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(x == FLIGHTSTATUS_FLIGHTMODE_POSITIONHOLD) ? FLIGHTMODE_GUIDANCE : \
(x == FLIGHTSTATUS_FLIGHTMODE_PATHPLANNER) ? FLIGHTMODE_GUIDANCE : FLIGHTMODE_UNDEFINED \
OP-329: Enumerate more possible flight modes now like multiple stabilization modes so that the FlightMode field is complete in terms of being informative enough git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2935 ebee16cc-31ac-478f-84a7-5cbb03baadba
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)
Flight/Modules: Corrected code to use tabs find ./flight/OpenPilot/Modules/ \! \( -name '*~' -a -prune \) -type f | xargs -I{} bash -c 'echo {}; dos2unix {}; gnuindent -npro -kr -i8 -ts8 -sob -ss -ncs -cp1 -il0 -hnl -l150 {};' git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1776 ebee16cc-31ac-478f-84a7-5cbb03baadba
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int32_t ManualControlInitialize();
OP-193: Weak leveling variant on rate mode. Slowly will return to level.
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/*
* These are assumptions we make in the flight code about the order of settings and their consistency between
* objects. Please keep this synchronized to the UAVObjects
*/
#define assumptions1 ( \
((int)MANUALCONTROLSETTINGS_STABILIZATION1SETTINGS_NONE == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_NONE) && \
((int)MANUALCONTROLSETTINGS_STABILIZATION1SETTINGS_RATE == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_RATE) && \
((int)MANUALCONTROLSETTINGS_STABILIZATION1SETTINGS_AXISLOCK == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_AXISLOCK) && \
((int)MANUALCONTROLSETTINGS_STABILIZATION1SETTINGS_WEAKLEVELING == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_WEAKLEVELING) && \
((int)MANUALCONTROLSETTINGS_STABILIZATION1SETTINGS_ATTITUDE == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_ATTITUDE) \
)
#define assumptions3 ( \
((int)MANUALCONTROLSETTINGS_STABILIZATION2SETTINGS_NONE == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_NONE) && \
((int)MANUALCONTROLSETTINGS_STABILIZATION2SETTINGS_RATE == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_RATE) && \
((int)MANUALCONTROLSETTINGS_STABILIZATION2SETTINGS_AXISLOCK == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_AXISLOCK) && \
((int)MANUALCONTROLSETTINGS_STABILIZATION2SETTINGS_WEAKLEVELING == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_WEAKLEVELING) && \
((int)MANUALCONTROLSETTINGS_STABILIZATION2SETTINGS_ATTITUDE == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_ATTITUDE) \
)
#define assumptions5 ( \
((int)MANUALCONTROLSETTINGS_STABILIZATION3SETTINGS_NONE == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_NONE) && \
((int)MANUALCONTROLSETTINGS_STABILIZATION3SETTINGS_RATE == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_RATE) && \
((int)MANUALCONTROLSETTINGS_STABILIZATION3SETTINGS_AXISLOCK == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_AXISLOCK) && \
((int)MANUALCONTROLSETTINGS_STABILIZATION3SETTINGS_WEAKLEVELING == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_WEAKLEVELING) && \
((int)MANUALCONTROLSETTINGS_STABILIZATION3SETTINGS_ATTITUDE == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_ATTITUDE) \
)
#define ARMING_CHANNEL_ROLL 0
#define ARMING_CHANNEL_PITCH 1
#define ARMING_CHANNEL_YAW 2
#define assumptions7 ( \
( ((int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)/2 == ARMING_CHANNEL_ROLL) && \
( ((int)MANUALCONTROLSETTINGS_ARMING_ROLLRIGHT -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)/2 == ARMING_CHANNEL_ROLL) && \
( ((int)MANUALCONTROLSETTINGS_ARMING_PITCHFORWARD -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)/2 == ARMING_CHANNEL_PITCH) && \
( ((int)MANUALCONTROLSETTINGS_ARMING_PITCHAFT -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)/2 == ARMING_CHANNEL_PITCH) && \
( ((int)MANUALCONTROLSETTINGS_ARMING_YAWLEFT -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)/2 == ARMING_CHANNEL_YAW) && \
( ((int)MANUALCONTROLSETTINGS_ARMING_YAWRIGHT -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)/2 == ARMING_CHANNEL_YAW) \
)
#define assumptions8 ( \
( ((int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)%2 == 0) && \
( ((int)MANUALCONTROLSETTINGS_ARMING_ROLLRIGHT -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)%2 != 0) && \
( ((int)MANUALCONTROLSETTINGS_ARMING_PITCHFORWARD -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)%2 == 0) && \
( ((int)MANUALCONTROLSETTINGS_ARMING_PITCHAFT -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)%2 != 0) && \
( ((int)MANUALCONTROLSETTINGS_ARMING_YAWLEFT -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)%2 == 0) && \
( ((int)MANUALCONTROLSETTINGS_ARMING_YAWRIGHT -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)%2 != 0) \
)
#define assumptions_flightmode ( \
( (int)MANUALCONTROLSETTINGS_FLIGHTMODEPOSITION_MANUAL == (int) FLIGHTSTATUS_FLIGHTMODE_MANUAL) && \
( (int)MANUALCONTROLSETTINGS_FLIGHTMODEPOSITION_STABILIZED1 == (int) FLIGHTSTATUS_FLIGHTMODE_STABILIZED1) && \
( (int)MANUALCONTROLSETTINGS_FLIGHTMODEPOSITION_STABILIZED2 == (int) FLIGHTSTATUS_FLIGHTMODE_STABILIZED2) && \
( (int)MANUALCONTROLSETTINGS_FLIGHTMODEPOSITION_STABILIZED3 == (int) FLIGHTSTATUS_FLIGHTMODE_STABILIZED3) && \
( (int)MANUALCONTROLSETTINGS_FLIGHTMODEPOSITION_VELOCITYCONTROL == (int) FLIGHTSTATUS_FLIGHTMODE_VELOCITYCONTROL) && \
( (int)MANUALCONTROLSETTINGS_FLIGHTMODEPOSITION_POSITIONHOLD == (int) FLIGHTSTATUS_FLIGHTMODE_POSITIONHOLD) \
)
UAVObjects: Space allocated in manualcontrolcommand did not match the number of channels in settings. Fixed this and added assertion to catch in future.
2011-09-09 08:17:13 +02:00
#define assumptions_channelcount ( \
( (int)MANUALCONTROLCOMMAND_CHANNEL_NUMELEM == (int)MANUALCONTROLSETTINGS_CHANNELGROUPS_NUMELEM ) && \
( (int)MANUALCONTROLCOMMAND_CHANNEL_NUMELEM == (int)MANUALCONTROLSETTINGS_CHANNELNUMBER_NUMELEM ) && \
( (int)MANUALCONTROLCOMMAND_CHANNEL_NUMELEM == (int)MANUALCONTROLSETTINGS_CHANNELMIN_NUMELEM ) && \
( (int)MANUALCONTROLCOMMAND_CHANNEL_NUMELEM == (int)MANUALCONTROLSETTINGS_CHANNELMAX_NUMELEM ) && \
( (int)MANUALCONTROLCOMMAND_CHANNEL_NUMELEM == (int)MANUALCONTROLSETTINGS_CHANNELNEUTRAL_NUMELEM ) )
Flight/Modules: Corrected code to use tabs find ./flight/OpenPilot/Modules/ \! \( -name '*~' -a -prune \) -type f | xargs -I{} bash -c 'echo {}; dos2unix {}; gnuindent -npro -kr -i8 -ts8 -sob -ss -ncs -cp1 -il0 -hnl -l150 {};' git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1776 ebee16cc-31ac-478f-84a7-5cbb03baadba
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#endif // MANUALCONTROL_H
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