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LibrePilot/flight/modules/ManualControl/inc/manualcontrol.h
abeck70 52147333ed OP-1769 Ground Support
1. Receiver.c for ground allows disabled channels for all but yaw and throttle
2. Reciever.c applies a deadband on throttle 0 position
3. Arming understands ground have a 0 throttle position
4. Actuator optimisations in general and fixes for mixing
5. Actuator mixer support for reversible motors
2015-03-10 22:54:51 +11:00

184 lines
6.2 KiB
C

/**
******************************************************************************
* @addtogroup OpenPilotModules OpenPilot Modules
* @{
* @addtogroup ManualControlModule Manual Control Module
* @{
*
* @file manualcontrol.h
* @author The OpenPilot Team, http://www.openpilot.org Copyright (C) 2014.
* @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
#include <openpilot.h>
#include <flightstatus.h>
#include <sanitycheck.h>
typedef void (*handlerFunc)(bool newinit);
typedef struct controlHandlerStruct {
FlightStatusControlChainData controlChain;
handlerFunc handler;
} controlHandler;
/**
* @brief Handler to interprete Command inputs in regards to arming/disarming (called in all flight modes)
* @input: ManualControlCommand, AccessoryDesired
* @output: FlightStatus.Arming
*/
void armHandler(bool newinit, FrameType_t frameType);
/**
* @brief Handler to control Manual flightmode - input directly steers actuators
* @input: ManualControlCommand
* @output: ActuatorDesired
*/
void manualHandler(bool newinit);
/**
* @brief Handler to control Stabilized flightmodes. FlightControl is governed by "Stabilization"
* @input: ManualControlCommand
* @output: StabilizationDesired
*/
void stabilizedHandler(bool newinit);
/**
* @brief Handler to control Guided flightmodes. FlightControl is governed by PathFollower, control via PathDesired
* @input: NONE: fully automated mode -- TODO recursively call handler for advanced stick commands
* @output: PathDesired
*/
void pathFollowerHandler(bool newinit);
/**
* @brief Handler to control Navigated flightmodes. FlightControl is governed by PathFollower, controlled indirectly via PathPlanner
* @input: NONE: fully automated mode -- TODO recursively call handler for advanced stick commands to affect navigation
* @output: NONE
*/
void pathPlannerHandler(bool newinit);
/**
* @brief Handler to setup takeofflocation on arming. it is set up during Arming
* @input: NONE:
* @output: NONE
*/
void takeOffLocationHandler();
/**
* @brief Initialize TakeoffLocationHanlder
*/
void takeOffLocationHandlerInit();
#define STABILIZATIONMODE_TABLE(ENTRY) \
ENTRY(MANUAL) \
ENTRY(RATE) \
ENTRY(ATTITUDE) \
ENTRY(AXISLOCK) \
ENTRY(WEAKLEVELING) \
ENTRY(VIRTUALBAR) \
ENTRY(ACRO) \
ENTRY(RATTITUDE) \
ENTRY(ALTITUDEHOLD) \
ENTRY(ALTITUDEVARIO) \
ENTRY(CRUISECONTROL)
#define EXPAND_FLIGHTSETTINGS_STAB1(x) ((int)FLIGHTMODESETTINGS_STABILIZATION1SETTINGS_##x == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_##x) &&
#define EXPAND_FLIGHTSETTINGS_STAB2(x) ((int)FLIGHTMODESETTINGS_STABILIZATION2SETTINGS_##x == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_##x) &&
#define EXPAND_FLIGHTSETTINGS_STAB3(x) ((int)FLIGHTMODESETTINGS_STABILIZATION3SETTINGS_##x == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_##x) &&
#define EXPAND_FLIGHTSETTINGS_STAB4(x) ((int)FLIGHTMODESETTINGS_STABILIZATION4SETTINGS_##x == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_##x) &&
#define EXPAND_FLIGHTSETTINGS_STAB5(x) ((int)FLIGHTMODESETTINGS_STABILIZATION5SETTINGS_##x == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_##x) &&
#define EXPAND_FLIGHTSETTINGS_STAB6(x) ((int)FLIGHTMODESETTINGS_STABILIZATION6SETTINGS_##x == (int)STABILIZATIONDESIRED_STABILIZATIONMODE_##x) &&
#define FLIGHTMODE_TABLE(ENTRY) \
ENTRY(MANUAL) \
ENTRY(STABILIZED1) \
ENTRY(STABILIZED2) \
ENTRY(STABILIZED3) \
ENTRY(STABILIZED4) \
ENTRY(STABILIZED5) \
ENTRY(STABILIZED6) \
ENTRY(POSITIONHOLD) \
ENTRY(RETURNTOBASE) \
ENTRY(LAND) \
ENTRY(PATHPLANNER) \
ENTRY(POI)
#define EXPAND_FLIGHTMODE(x) ((int)FLIGHTMODESETTINGS_FLIGHTMODEPOSITION_##x == (int)FLIGHTSTATUS_FLIGHTMODE_##x) &&
/*
* 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 \
( \
STABILIZATIONMODE_TABLE(EXPAND_FLIGHTSETTINGS_STAB1) \
1 \
)
#define assumptions2 \
( \
STABILIZATIONMODE_TABLE(EXPAND_FLIGHTSETTINGS_STAB2) \
1 \
)
#define assumptions3 \
( \
STABILIZATIONMODE_TABLE(EXPAND_FLIGHTSETTINGS_STAB3) \
1 \
)
#define assumptions4 \
( \
STABILIZATIONMODE_TABLE(EXPAND_FLIGHTSETTINGS_STAB4) \
1 \
)
#define assumptions5 \
( \
STABILIZATIONMODE_TABLE(EXPAND_FLIGHTSETTINGS_STAB5) \
1 \
)
#define assumptions6 \
( \
STABILIZATIONMODE_TABLE(EXPAND_FLIGHTSETTINGS_STAB6) \
1 \
)
#define assumptions7 \
( \
((int)FLIGHTMODESETTINGS_STABILIZATION1SETTINGS_NUMELEM == (int)FLIGHTMODESETTINGS_STABILIZATION2SETTINGS_NUMELEM) && \
((int)FLIGHTMODESETTINGS_STABILIZATION1SETTINGS_NUMELEM == (int)FLIGHTMODESETTINGS_STABILIZATION3SETTINGS_NUMELEM) && \
((int)FLIGHTMODESETTINGS_STABILIZATION1SETTINGS_NUMELEM == (int)FLIGHTMODESETTINGS_STABILIZATION4SETTINGS_NUMELEM) && \
((int)FLIGHTMODESETTINGS_STABILIZATION1SETTINGS_NUMELEM == (int)FLIGHTMODESETTINGS_STABILIZATION5SETTINGS_NUMELEM) && \
((int)FLIGHTMODESETTINGS_STABILIZATION1SETTINGS_NUMELEM == (int)FLIGHTMODESETTINGS_STABILIZATION6SETTINGS_NUMELEM) && \
1 \
)
#define assumptions_flightmode \
( \
FLIGHTMODE_TABLE(EXPAND_FLIGHTMODE) \
1 \
)
#endif // MANUALCONTROL_H