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116 lines
6.9 KiB
C
116 lines
6.9 KiB
C
/**
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******************************************************************************
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* @addtogroup OpenPilotModules OpenPilot Modules
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* @{
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* @addtogroup ManualControlModule Manual Control Module
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* @{
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*
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* @file manualcontrol.h
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* @author The OpenPilot Team, http://www.openpilot.org Copyright (C) 2010.
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* @brief ManualControl module. Handles safety R/C link and flight mode.
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*
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* @see The GNU Public License (GPL) Version 3
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*
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*****************************************************************************/
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/*
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* This program is free software; you can redistribute it and/or modify
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* it under the terms of the GNU General Public License as published by
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* the Free Software Foundation; either version 3 of the License, or
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* (at your option) any later version.
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*
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* This program is distributed in the hope that it will be useful, but
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* WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY
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* or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
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* for more details.
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*
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* You should have received a copy of the GNU General Public License along
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* with this program; if not, write to the Free Software Foundation, Inc.,
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* 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA
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*/
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#ifndef MANUALCONTROL_H
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#define MANUALCONTROL_H
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#include "manualcontrolcommand.h"
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typedef enum {FLIGHTMODE_UNDEFINED = 0, FLIGHTMODE_MANUAL = 1, FLIGHTMODE_STABILIZED = 2, FLIGHTMODE_GUIDANCE = 3} flightmode_path;
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#define PARSE_FLIGHT_MODE(x) ( \
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(x == FLIGHTSTATUS_FLIGHTMODE_MANUAL) ? FLIGHTMODE_MANUAL : \
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(x == FLIGHTSTATUS_FLIGHTMODE_STABILIZED1) ? FLIGHTMODE_STABILIZED : \
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(x == FLIGHTSTATUS_FLIGHTMODE_STABILIZED2) ? FLIGHTMODE_STABILIZED : \
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(x == FLIGHTSTATUS_FLIGHTMODE_STABILIZED3) ? FLIGHTMODE_STABILIZED : \
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(x == FLIGHTSTATUS_FLIGHTMODE_VELOCITYCONTROL) ? FLIGHTMODE_GUIDANCE : \
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(x == FLIGHTSTATUS_FLIGHTMODE_POSITIONHOLD) ? FLIGHTMODE_GUIDANCE : FLIGHTMODE_UNDEFINED \
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)
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int32_t ManualControlInitialize();
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/*
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* These are assumptions we make in the flight code about the order of settings and their consistency between
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* objects. Please keep this synchronized to the UAVObjects
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*/
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#define assumptions1 ( \
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((int)MANUALCONTROLSETTINGS_STABILIZATION1SETTINGS_NONE == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_NONE) && \
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((int)MANUALCONTROLSETTINGS_STABILIZATION1SETTINGS_RATE == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_RATE) && \
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((int)MANUALCONTROLSETTINGS_STABILIZATION1SETTINGS_AXISLOCK == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_AXISLOCK) && \
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((int)MANUALCONTROLSETTINGS_STABILIZATION1SETTINGS_WEAKLEVELING == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_WEAKLEVELING) && \
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((int)MANUALCONTROLSETTINGS_STABILIZATION1SETTINGS_ATTITUDE == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_ATTITUDE) \
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)
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#define assumptions3 ( \
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((int)MANUALCONTROLSETTINGS_STABILIZATION2SETTINGS_NONE == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_NONE) && \
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((int)MANUALCONTROLSETTINGS_STABILIZATION2SETTINGS_RATE == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_RATE) && \
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((int)MANUALCONTROLSETTINGS_STABILIZATION2SETTINGS_AXISLOCK == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_AXISLOCK) && \
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((int)MANUALCONTROLSETTINGS_STABILIZATION2SETTINGS_WEAKLEVELING == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_WEAKLEVELING) && \
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((int)MANUALCONTROLSETTINGS_STABILIZATION2SETTINGS_ATTITUDE == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_ATTITUDE) \
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)
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#define assumptions5 ( \
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((int)MANUALCONTROLSETTINGS_STABILIZATION3SETTINGS_NONE == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_NONE) && \
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((int)MANUALCONTROLSETTINGS_STABILIZATION3SETTINGS_RATE == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_RATE) && \
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((int)MANUALCONTROLSETTINGS_STABILIZATION3SETTINGS_AXISLOCK == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_AXISLOCK) && \
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((int)MANUALCONTROLSETTINGS_STABILIZATION3SETTINGS_WEAKLEVELING == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_WEAKLEVELING) && \
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((int)MANUALCONTROLSETTINGS_STABILIZATION3SETTINGS_ATTITUDE == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_ATTITUDE) \
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)
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#define ARMING_CHANNEL_ROLL 0
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#define ARMING_CHANNEL_PITCH 1
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#define ARMING_CHANNEL_YAW 2
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#define assumptions7 ( \
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( ((int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)/2 == ARMING_CHANNEL_ROLL) && \
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( ((int)MANUALCONTROLSETTINGS_ARMING_ROLLRIGHT -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)/2 == ARMING_CHANNEL_ROLL) && \
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( ((int)MANUALCONTROLSETTINGS_ARMING_PITCHFORWARD -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)/2 == ARMING_CHANNEL_PITCH) && \
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( ((int)MANUALCONTROLSETTINGS_ARMING_PITCHAFT -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)/2 == ARMING_CHANNEL_PITCH) && \
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( ((int)MANUALCONTROLSETTINGS_ARMING_YAWLEFT -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)/2 == ARMING_CHANNEL_YAW) && \
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( ((int)MANUALCONTROLSETTINGS_ARMING_YAWRIGHT -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)/2 == ARMING_CHANNEL_YAW) \
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)
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#define assumptions8 ( \
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( ((int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)%2 == 0) && \
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( ((int)MANUALCONTROLSETTINGS_ARMING_ROLLRIGHT -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)%2 != 0) && \
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( ((int)MANUALCONTROLSETTINGS_ARMING_PITCHFORWARD -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)%2 == 0) && \
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( ((int)MANUALCONTROLSETTINGS_ARMING_PITCHAFT -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)%2 != 0) && \
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( ((int)MANUALCONTROLSETTINGS_ARMING_YAWLEFT -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)%2 == 0) && \
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( ((int)MANUALCONTROLSETTINGS_ARMING_YAWRIGHT -(int)MANUALCONTROLSETTINGS_ARMING_ROLLLEFT)%2 != 0) \
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)
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#define assumptions_flightmode ( \
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( (int)MANUALCONTROLSETTINGS_FLIGHTMODEPOSITION_MANUAL == (int) FLIGHTSTATUS_FLIGHTMODE_MANUAL) && \
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( (int)MANUALCONTROLSETTINGS_FLIGHTMODEPOSITION_STABILIZED1 == (int) FLIGHTSTATUS_FLIGHTMODE_STABILIZED1) && \
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( (int)MANUALCONTROLSETTINGS_FLIGHTMODEPOSITION_STABILIZED2 == (int) FLIGHTSTATUS_FLIGHTMODE_STABILIZED2) && \
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( (int)MANUALCONTROLSETTINGS_FLIGHTMODEPOSITION_STABILIZED3 == (int) FLIGHTSTATUS_FLIGHTMODE_STABILIZED3) && \
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( (int)MANUALCONTROLSETTINGS_FLIGHTMODEPOSITION_VELOCITYCONTROL == (int) FLIGHTSTATUS_FLIGHTMODE_VELOCITYCONTROL) && \
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( (int)MANUALCONTROLSETTINGS_FLIGHTMODEPOSITION_POSITIONHOLD == (int) FLIGHTSTATUS_FLIGHTMODE_POSITIONHOLD) \
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)
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#define assumptions_channelcount ( \
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( (int)MANUALCONTROLCOMMAND_CHANNEL_NUMELEM == (int)MANUALCONTROLSETTINGS_CHANNELGROUPS_NUMELEM ) && \
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( (int)MANUALCONTROLCOMMAND_CHANNEL_NUMELEM == (int)MANUALCONTROLSETTINGS_CHANNELNUMBER_NUMELEM ) && \
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( (int)MANUALCONTROLCOMMAND_CHANNEL_NUMELEM == (int)MANUALCONTROLSETTINGS_CHANNELMIN_NUMELEM ) && \
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( (int)MANUALCONTROLCOMMAND_CHANNEL_NUMELEM == (int)MANUALCONTROLSETTINGS_CHANNELMAX_NUMELEM ) && \
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( (int)MANUALCONTROLCOMMAND_CHANNEL_NUMELEM == (int)MANUALCONTROLSETTINGS_CHANNELNEUTRAL_NUMELEM ) )
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#endif // MANUALCONTROL_H
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