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flightgear/src/Autopilot/newauto.hxx

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// newauto.hxx -- autopilot defines and prototypes (very alpha)
//
// Started April 1998 Copyright (C) 1998
//
// Contributions by Jeff Goeke-Smith <jgoeke@voyager.net>
// Norman Vine <nhv@cape.com>
// Curtis Olson <curt@flightgear.org>
//
// 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 2 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., 675 Mass Ave, Cambridge, MA 02139, USA.
//
// $Id$
#ifndef _NEWAUTO_HXX
#define _NEWAUTO_HXX
// Structures
class FGAutopilot {
public:
enum fgAutoHeadingMode {
FG_HEADING_LOCK = 0,
FG_HEADING_NAV1 = 1,
FG_HEADING_NAV2 = 2,
FG_HEADING_WAYPOINT = 3
};
enum fgAutoAltitudeMode {
FG_ALTITUDE_LOCK = 0,
FG_ALTITUDE_TERRAIN = 1,
FG_ALTITUDE_GS1 = 2,
FG_ALTITUDE_GS2 = 3
};
private:
bool heading_hold; // the current state of the heading hold
bool altitude_hold; // the current state of the altitude hold
bool auto_throttle; // the current state of the auto throttle
fgAutoHeadingMode heading_mode;
fgAutoAltitudeMode altitude_mode;
double TargetLatitude; // the latitude the AP should steer to.
double TargetLongitude; // the longitude the AP should steer to.
double TargetDistance; // the distance to Target.
double TargetHeading; // the heading the AP should steer to.
double TargetAltitude; // altitude to hold
double TargetAGL; // the terrain separation
double TargetClimbRate; // climb rate to shoot for
double TargetSpeed; // speed to shoot for
double alt_error_accum; // altitude error accumulator
double climb_error_accum; // climb error accumulator (for GS)
double speed_error_accum; // speed error accumulator
double TargetSlope; // the glide slope hold value
double MaxRoll ; // the max the plane can roll for the turn
double RollOut; // when the plane should roll out
// measured from Heading
double MaxAileron; // how far to move the aleroin from center
double RollOutSmooth; // deg to use for smoothing Aileron Control
double MaxElevator; // the maximum elevator allowed
double SlopeSmooth; // smoothing angle for elevator
// following for testing disengagement of autopilot upon pilot
// interaction with controls
double old_aileron;
double old_elevator;
double old_elevator_trim;
double old_rudder;
// manual controls override beyond this value
double disengage_threshold;
// For future cross track error adjust
double old_lat;
double old_lon;
// keeping these locally to save work inside main loop
char TargetLatitudeStr[64];
char TargetLongitudeStr[64];
char TargetLatLonStr[64];
char TargetDistanceStr[64];
char TargetHeadingStr[64];
char TargetAltitudeStr[64];
public:
// Initialize autopilot system
void init();
// Reset the autopilot system
void reset(void);
// run an interation of the autopilot (updates control positions)
int run();
void AltitudeSet( double new_altitude );
void AltitudeAdjust( double inc );
void HeadingAdjust( double inc );
void AutoThrottleAdjust( double inc );
void HeadingSet( double value );
inline bool get_HeadingEnabled() const { return heading_hold; }
inline void set_HeadingEnabled( bool value ) { heading_hold = value; }
inline fgAutoHeadingMode get_HeadingMode() const { return heading_mode; }
void set_HeadingMode( fgAutoHeadingMode mode );
inline bool get_AltitudeEnabled() const { return altitude_hold; }
inline void set_AltitudeEnabled( bool value ) { altitude_hold = value; }
inline fgAutoAltitudeMode get_AltitudeMode() const { return altitude_mode;}
void set_AltitudeMode( fgAutoAltitudeMode mode );
inline bool get_AutoThrottleEnabled() const { return auto_throttle; }
void set_AutoThrottleEnabled( bool value );
inline double get_TargetLatitude() const { return TargetLatitude; }
inline void set_TargetLatitude( double val ) { TargetLatitude = val; }
inline void set_old_lat( double val ) { old_lat = val; }
inline double get_TargetLongitude() const { return TargetLongitude; }
inline void set_TargetLongitude( double val ) { TargetLongitude = val; }
inline void set_old_lon( double val ) { old_lon = val; }
inline double get_TargetHeading() const { return TargetHeading; }
inline void set_TargetHeading( double val ) { TargetHeading = val; }
inline double get_TargetDistance() const { return TargetDistance; }
inline void set_TargetDistance( double val ) { TargetDistance = val; }
inline double get_TargetAltitude() const { return TargetAltitude; }
inline void set_TargetAltitude( double val ) { TargetAltitude = val; }
inline char *get_TargetLatitudeStr() { return TargetLatitudeStr; }
inline char *get_TargetLongitudeStr() { return TargetLongitudeStr; }
inline char *get_TargetDistanceStr() { return TargetDistanceStr; }
inline char *get_TargetHeadingStr() { return TargetHeadingStr; }
inline char *get_TargetAltitudeStr() { return TargetAltitudeStr; }
inline char *get_TargetLatLonStr() { return TargetLatLonStr; }
// utility functions
void MakeTargetLatLonStr( double lat, double lon );
void MakeTargetAltitudeStr( double altitude );
void MakeTargetHeadingStr( double bearing );
void MakeTargetDistanceStr( double distance );
void update_old_control_values();
// accessors
inline double get_MaxRoll() const { return MaxRoll; }
inline void set_MaxRoll( double val ) { MaxRoll = val; }
inline double get_RollOut() const { return RollOut; }
inline void set_RollOut( double val ) { RollOut = val; }
inline double get_MaxAileron() const { return MaxAileron; }
inline void set_MaxAileron( double val ) { MaxAileron = val; }
inline double get_RollOutSmooth() const { return RollOutSmooth; }
inline void set_RollOutSmooth( double val ) { RollOutSmooth = val; }
};
extern FGAutopilot *current_autopilot;
#endif // _NEWAUTO_HXX