2000-04-30 06:51:49 +00:00
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// newauto.hxx -- autopilot defines and prototypes (very alpha)
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//
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// Started April 1998 Copyright (C) 1998
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//
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// Contributions by Jeff Goeke-Smith <jgoeke@voyager.net>
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// Norman Vine <nhv@cape.com>
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// Curtis Olson <curt@flightgear.org>
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//
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// This program is free software; you can redistribute it and/or
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// modify it under the terms of the GNU General Public License as
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// published by the Free Software Foundation; either version 2 of the
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// License, or (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
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// MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
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// General Public License for more details.
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//
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// You should have received a copy of the GNU General Public License
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// along with this program; if not, write to the Free Software
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// Foundation, Inc., 675 Mass Ave, Cambridge, MA 02139, USA.
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//
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// $Id$
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#ifndef _NEWAUTO_HXX
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#define _NEWAUTO_HXX
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2000-10-11 00:18:26 +00:00
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#include <simgear/route/waypoint.hxx>
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2000-04-30 06:51:49 +00:00
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// Structures
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class FGAutopilot {
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public:
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enum fgAutoHeadingMode {
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FG_HEADING_LOCK = 0,
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2000-04-30 22:21:47 +00:00
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FG_HEADING_NAV1 = 1,
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FG_HEADING_NAV2 = 2,
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FG_HEADING_WAYPOINT = 3
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2000-04-30 06:51:49 +00:00
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};
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enum fgAutoAltitudeMode {
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FG_ALTITUDE_LOCK = 0,
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FG_ALTITUDE_TERRAIN = 1,
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FG_ALTITUDE_GS1 = 2,
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FG_ALTITUDE_GS2 = 3
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};
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private:
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bool heading_hold; // the current state of the heading hold
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bool altitude_hold; // the current state of the altitude hold
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bool auto_throttle; // the current state of the auto throttle
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fgAutoHeadingMode heading_mode;
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fgAutoAltitudeMode altitude_mode;
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2000-10-11 00:18:26 +00:00
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SGWayPoint waypoint; // the waypoint the AP should steer to.
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// double TargetLatitude; // the latitude the AP should steer to.
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// double TargetLongitude; // the longitude the AP should steer to.
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2000-04-30 06:51:49 +00:00
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double TargetDistance; // the distance to Target.
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double TargetHeading; // the heading the AP should steer to.
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double TargetAltitude; // altitude to hold
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double TargetAGL; // the terrain separation
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double TargetClimbRate; // climb rate to shoot for
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double TargetSpeed; // speed to shoot for
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double alt_error_accum; // altitude error accumulator
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2000-04-30 22:21:47 +00:00
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double climb_error_accum; // climb error accumulator (for GS)
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2000-04-30 06:51:49 +00:00
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double speed_error_accum; // speed error accumulator
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double TargetSlope; // the glide slope hold value
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double MaxRoll ; // the max the plane can roll for the turn
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double RollOut; // when the plane should roll out
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// measured from Heading
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double MaxAileron; // how far to move the aleroin from center
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double RollOutSmooth; // deg to use for smoothing Aileron Control
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double MaxElevator; // the maximum elevator allowed
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double SlopeSmooth; // smoothing angle for elevator
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// following for testing disengagement of autopilot upon pilot
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// interaction with controls
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double old_aileron;
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double old_elevator;
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double old_elevator_trim;
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double old_rudder;
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// manual controls override beyond this value
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double disengage_threshold;
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// For future cross track error adjust
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double old_lat;
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double old_lon;
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// keeping these locally to save work inside main loop
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char TargetLatitudeStr[64];
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char TargetLongitudeStr[64];
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char TargetLatLonStr[64];
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char TargetDistanceStr[64];
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char TargetHeadingStr[64];
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char TargetAltitudeStr[64];
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public:
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// Initialize autopilot system
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void init();
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// Reset the autopilot system
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void reset(void);
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// run an interation of the autopilot (updates control positions)
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int run();
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void AltitudeSet( double new_altitude );
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void AltitudeAdjust( double inc );
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void HeadingAdjust( double inc );
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void AutoThrottleAdjust( double inc );
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void HeadingSet( double value );
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inline bool get_HeadingEnabled() const { return heading_hold; }
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inline void set_HeadingEnabled( bool value ) { heading_hold = value; }
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inline fgAutoHeadingMode get_HeadingMode() const { return heading_mode; }
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void set_HeadingMode( fgAutoHeadingMode mode );
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inline bool get_AltitudeEnabled() const { return altitude_hold; }
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inline void set_AltitudeEnabled( bool value ) { altitude_hold = value; }
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inline fgAutoAltitudeMode get_AltitudeMode() const { return altitude_mode;}
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void set_AltitudeMode( fgAutoAltitudeMode mode );
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inline bool get_AutoThrottleEnabled() const { return auto_throttle; }
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void set_AutoThrottleEnabled( bool value );
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2000-10-11 00:18:26 +00:00
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inline void set_WayPoint( const double lon, const double lat,
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const string s ) {
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waypoint = SGWayPoint( lon, lat, SGWayPoint::WGS84, "Current WP" );
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}
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inline double get_TargetLatitude() const {
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return waypoint.get_target_lat();
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}
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inline double get_TargetLongitude() const {
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return waypoint.get_target_lon();
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}
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// inline void set_TargetLatitude( double val ) { TargetLatitude = val; }
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// inline void set_TargetLongitude( double val ) { TargetLongitude = val; }
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2000-04-30 06:51:49 +00:00
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inline void set_old_lat( double val ) { old_lat = val; }
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inline void set_old_lon( double val ) { old_lon = val; }
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inline double get_TargetHeading() const { return TargetHeading; }
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inline void set_TargetHeading( double val ) { TargetHeading = val; }
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inline double get_TargetDistance() const { return TargetDistance; }
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inline void set_TargetDistance( double val ) { TargetDistance = val; }
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inline double get_TargetAltitude() const { return TargetAltitude; }
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inline void set_TargetAltitude( double val ) { TargetAltitude = val; }
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inline char *get_TargetLatitudeStr() { return TargetLatitudeStr; }
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inline char *get_TargetLongitudeStr() { return TargetLongitudeStr; }
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inline char *get_TargetDistanceStr() { return TargetDistanceStr; }
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inline char *get_TargetHeadingStr() { return TargetHeadingStr; }
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inline char *get_TargetAltitudeStr() { return TargetAltitudeStr; }
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inline char *get_TargetLatLonStr() { return TargetLatLonStr; }
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// utility functions
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void MakeTargetLatLonStr( double lat, double lon );
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void MakeTargetAltitudeStr( double altitude );
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void MakeTargetHeadingStr( double bearing );
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void MakeTargetDistanceStr( double distance );
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void update_old_control_values();
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// accessors
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inline double get_MaxRoll() const { return MaxRoll; }
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inline void set_MaxRoll( double val ) { MaxRoll = val; }
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inline double get_RollOut() const { return RollOut; }
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inline void set_RollOut( double val ) { RollOut = val; }
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inline double get_MaxAileron() const { return MaxAileron; }
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inline void set_MaxAileron( double val ) { MaxAileron = val; }
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inline double get_RollOutSmooth() const { return RollOutSmooth; }
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inline void set_RollOutSmooth( double val ) { RollOutSmooth = val; }
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};
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extern FGAutopilot *current_autopilot;
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#endif // _NEWAUTO_HXX
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