/*
This program (files gps.c and gps.h) is free software; you can redistribute it and/or modify
it under the terms of the GNU Lesser 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 and GNU Lesser General Public License for more details.
You should have received a copy of GNU General Public License (License_GPL.txt) and
GNU Lesser General Public License (License_LGPL.txt) along with this program.
If not, see <http://www.gnu.org/licenses/>.
Please note: All the other files for the project "Mikrokopter" by H.Buss are under the license (license_buss.txt) published by www.mikrokopter.de
*/
/*++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
von Peter Muehlenbrock alias Salvo
Auswertung der Daten vom GPS im ublox Format
Hold Modus mit PID Regler
Rückstuerz zur Basis Funktion
Stand 14.1.2008
++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
*/
#include "main.h"
#include "math.h"
//#include "gps.h"
// Defines fuer ublox Messageformat um Auswertung zu steuern
#define UBLOX_IDLE 0
#define UBLOX_SYNC1 1
#define UBLOX_SYNC2 2
#define UBLOX_CLASS 3
#define UBLOX_ID 4
#define UBLOX_LEN1 5
#define UBLOX_LEN2 6
#define UBLOX_CKA 7
#define UBLOX_CKB 8
#define UBLOX_PAYLOAD 9
// ublox Protokoll Identifier
#define UBLOX_NAV_POSUTM 0x08
#define UBLOX_NAV_STATUS 0x03
#define UBLOX_NAV_VELED 0x12
#define UBLOX_NAV_CLASS 0x01
#define UBLOX_SYNCH1_CHAR 0xB5
#define UBLOX_SYNCH2_CHAR 0x62
signed int GPS_Nick
= 0;
signed int GPS_Roll
= 0;
short int ublox_msg_state
= UBLOX_IDLE
;
static uint8_t chk_a
=0; //Checksum
static uint8_t chk_b
=0;
short int gps_state
,gps_sub_state
; //Zustaende der Statemachine
short int gps_updte_flag
;
static long signed gps_reg_x
,gps_reg_y
;
static unsigned int rx_len
;
static unsigned int ptr_payload_data_end
;
unsigned int gps_alive_cnt
; // Wird bei jedem gueltigen GPS Telegramm hochgezaehlt
static signed int hdng_2home
,dist_2home
; //Richtung und Entfernung zur home Position
static signed gps_tick
; //wird bei jedem Update durch das GPS Modul hochgezaehlt
static short int hold_fast
,hold_reset_int
; //Flags fuer Hold Regler
static uint8_t *ptr_payload_data
;
static uint8_t *ptr_pac_status
;
static int dist_flown
;
static unsigned int int_ovfl_cnt
; // Zaehler fuer Overflows des Integrators
static int gps_quiet_cnt
; // zaheler fuer GPS Off Time beim Kameraausloesen
short int Get_GPS_data
(void);
NAV_POSUTM_t actual_pos
; // Aktuelle Nav Daten werden hier im ublox Format abgelegt
NAV_STATUS_t actual_status
; // Aktueller Nav Status
NAV_VELNED_t actual_speed
; // Aktueller Geschwindigkeits und Richtungsdaten
GPS_ABS_POSITION_t gps_act_position
; // Alle wichtigen Daten zusammengefasst
GPS_ABS_POSITION_t gps_home_position
; // Die Startposition, beim Kalibrieren ermittelt
GPS_REL_POSITION_t gps_rel_act_position
; // Die aktuelle relative Position bezogen auf Home Position
GPS_REL_POSITION_t gps_rel_hold_position
; // Die gespeicherte Sollposition fuer GPS_ Hold Mode
GPS_REL_POSITION_t gps_rel_start_position
; // Die gespeicherte Ausgangsposition fuer GPS_ Home Mode
// Initialisierung
void GPS_Neutral
(void)
{
ublox_msg_state
= UBLOX_IDLE
;
gps_state
= GPS_CRTL_IDLE
;
gps_sub_state
= GPS_CRTL_IDLE
;
actual_pos.
status = 0;
actual_speed.
status = 0;
actual_status.
status = 0;
gps_home_position.
status = 0; // Noch keine gueltige Home Position
gps_act_position.
status = 0;
gps_rel_act_position.
status = 0;
GPS_Nick
= 0;
GPS_Roll
= 0;
gps_updte_flag
= 0;
gps_alive_cnt
= 0;
}
// Home Position sichern falls Daten verfuegbar sind.
void GPS_Save_Home
(void)
{
short int n
;
n
= Get_GPS_data
();
if (n
== 0) // Gueltige und aktuelle Daten ?
{
// Neue GPS Daten liegen vor
gps_home_position.
utm_east = gps_act_position.
utm_east;
gps_home_position.
utm_north = gps_act_position.
utm_north;
gps_home_position.
utm_alt = gps_act_position.
utm_alt;
gps_home_position.
status = 1; // Home Position gueltig
}
}
// Relative Position zur Home Position bestimmen
// Rueckgabewert 0= Daten sind aktuell und gueltig. 1= Keine Aenderung. 2= Daten ungueltig
short int Get_Rel_Position
(void)
{
short int n
= 0;
n
= Get_GPS_data
();
if (n
>=1) return (n
); // nix zu tun, weil keine neue Daten da sind
if (gps_alive_cnt
< 1000) gps_alive_cnt
+= 600; // Timeoutzaehler. Wird in Motorregler Routine ueberwacht und dekrementiert
if (gps_home_position.
status > 0) //Nur wenn Home Position vorliegt
{
gps_rel_act_position.
utm_east = (int) (gps_act_position.
utm_east - gps_home_position.
utm_east);
gps_rel_act_position.
utm_north = (int) (gps_act_position.
utm_north - gps_home_position.
utm_north);
gps_rel_act_position.
utm_alt = (int) (gps_act_position.
utm_alt - gps_home_position.
utm_alt);
gps_rel_act_position.
status = 1; // gueltige Positionsdaten
n
= 0;
gps_updte_flag
= 1; // zeigt an, dass neue Daten vorliegen.
}
else
{
n
= 2; //keine gueltigen Daten vorhanden
gps_rel_act_position.
status = 0; //keine gueltige Position weil keine home Position da ist.
}
return (n
);
}
// Daten aus aktuellen ublox Messages extrahieren
// Rueckgabewert 0= Daten sind aktuell und gueltig. 1= Keine Aenderung. 2= Daten ungueltig
short int Get_GPS_data
(void)
{
short int n
= 1;
if (actual_pos.
status == 0) return (1); //damit es schnell geht, wenn nix zu tun ist
if ((actual_pos.
status > 0) && (actual_status.
status > 0) && (actual_speed.
status > 0))
{
if (((actual_status.
gpsfix_type & 0x03) >=2) && ((actual_status.
nav_status_flag & 0x01) >=1)) // nur wenn Daten aktuell und gueltig sind
{
actual_status.
status = 0;
gps_act_position.
utm_east = actual_pos.
utm_east/10;
gps_act_position.
utm_north = actual_pos.
utm_north/10;
gps_act_position.
utm_alt = actual_pos.
utm_alt/10;
actual_pos.
status = 0; //neue ublox Messages anfordern
gps_act_position.
speed_gnd = actual_speed.
speed_gnd;
gps_act_position.
speed_gnd = actual_speed.
speed_gnd;
gps_act_position.
heading = actual_speed.
heading/100000;
actual_speed.
status = 0;
gps_act_position.
status = 1;
n
= 0; //Daten gueltig
}
else
{
gps_act_position.
status = 0; //Keine gueltigen Daten
actual_speed.
status = 0;
actual_status.
status = 0;
actual_pos.
status = 0; //neue ublox Messages anfordern
n
= 2;
}
}
return (n
);
}
/*
Daten vom GPS im ublox MSG Format auswerten
Die Routine wird bei jedem Empfang eines Zeichens vom GPS Modul durch den UART IRQ aufgerufen
// Die UBX Messages NAV_POSUTM, NAV_STATUS und NAV_VALED muessen aktiviert sein
*/
void Get_Ublox_Msg
(uint8_t rx
)
{
switch (ublox_msg_state
)
{
case UBLOX_IDLE
: // Zuerst Synchcharacters pruefen
if ( rx
== UBLOX_SYNCH1_CHAR
) ublox_msg_state
= UBLOX_SYNC1
;
else ublox_msg_state
= UBLOX_IDLE
;
break;
case UBLOX_SYNC1
:
if (rx
== UBLOX_SYNCH2_CHAR
) ublox_msg_state
= UBLOX_SYNC2
;
else ublox_msg_state
= UBLOX_IDLE
;
chk_a
= 0,chk_b
= 0;
break;
case UBLOX_SYNC2
:
if (rx
== UBLOX_NAV_CLASS
) ublox_msg_state
= UBLOX_CLASS
;
else ublox_msg_state
= UBLOX_IDLE
;
break;
case UBLOX_CLASS
: // Nur NAV Meldungen auswerten
switch (rx
)
{
case UBLOX_NAV_POSUTM
:
ptr_pac_status
= &actual_pos.
status;
if (*ptr_pac_status
> 0) ublox_msg_state
= UBLOX_IDLE
; //Abbruch weil Daten noch nicht verwendet wurden
else
{
ptr_payload_data
= &actual_pos
;
ptr_payload_data_end
= &actual_pos.
status;
ublox_msg_state
= UBLOX_LEN1
;
}
break;
case UBLOX_NAV_STATUS
:
ptr_pac_status
= &actual_status.
status;
if (*ptr_pac_status
> 0) ublox_msg_state
= UBLOX_IDLE
;
else
{
ptr_payload_data
= &actual_status
;
ptr_payload_data_end
= &actual_status.
status;
ublox_msg_state
= UBLOX_LEN1
;
}
break;
case UBLOX_NAV_VELED
:
ptr_pac_status
= &actual_speed.
status;
if (*ptr_pac_status
> 0) ublox_msg_state
= UBLOX_IDLE
;
else
{
ptr_payload_data
= &actual_speed
;
ptr_payload_data_end
= &actual_speed.
status;
ublox_msg_state
= UBLOX_LEN1
;
}
break;
default:
ublox_msg_state
= UBLOX_IDLE
;
break;
}
chk_a
= UBLOX_NAV_CLASS
+ rx
;
chk_b
= UBLOX_NAV_CLASS
+ chk_a
;
break;
case UBLOX_LEN1
: // Laenge auswerten
rx_len
= rx
;
chk_a
+= rx
;
chk_b
+= chk_a
;
ublox_msg_state
= UBLOX_LEN2
;
break;
case UBLOX_LEN2
: // Laenge auswerten
rx_len
= rx_len
+ (rx
*256); // Laenge ermitteln
chk_a
+= rx
;
chk_b
+= chk_a
;
ublox_msg_state
= UBLOX_PAYLOAD
;
break;
case UBLOX_PAYLOAD
: // jetzt Nutzdaten einlesen
if (rx_len
> 0)
{
*ptr_payload_data
= rx
;
chk_a
+= rx
;
chk_b
+= chk_a
;
--rx_len
;
if ((rx_len
> 0) && (ptr_payload_data
<= ptr_payload_data_end
))
{
ptr_payload_data
++;
ublox_msg_state
= UBLOX_PAYLOAD
;
}
else ublox_msg_state
= UBLOX_CKA
;
}
else ublox_msg_state
= UBLOX_IDLE
; // Abbruch wegen Fehler
break;
case UBLOX_CKA
: // Checksum pruefen
if (rx
== chk_a
) ublox_msg_state
= UBLOX_CKB
;
else ublox_msg_state
= UBLOX_IDLE
; // Abbruch wegen Fehler
break;
case UBLOX_CKB
: // Checksum pruefen
if (rx
== chk_b
) *ptr_pac_status
= 1; // Paket ok
ublox_msg_state
= UBLOX_IDLE
;
break;
default:
ublox_msg_state
= UBLOX_IDLE
;
break;
}
}
//Zentrale Statemachine fuer alle GPS relevanten Regelungsablauefe
short int GPS_CRTL
(short int cmd
)
{
static unsigned int cnt
; // Zaehler fuer diverse Verzoegerungen
static long int delta_north
,delta_east
; // Mass fuer Distanz zur Sollposition
signed int n
;
static signed int gps_g2t_act_v
; // Aktuelle Geschwindigkeitsvorgabe fuer Home Funktion
signed int dist_frm_start_east
,dist_frm_start_north
;
int amplfy_speed_east
,amplfy_speed_north
; //Verstaerkungsfaktoren fuer D-Anteil
static signed int int_east
,int_north
; //Integrierer
long int speed_east
,speed_north
; //Aktuelle Geschwindigkeit
signed long int_east1
,int_north1
;
int dist_east
,dist_north
;
int diff_p
; //Vom Modus abhaengige zusaetzliche Verstaerkung
long ni
,ro
; // Nick und Roll Zwischenwerte
switch (cmd
)
{
case GPS_CMD_REQ_HOME
: // Es soll zum Startpunkt zurueckgeflogen werden.
if ((gps_state
!= GPS_CRTL_HOLD_ACTIVE
) && (gps_state
!= GPS_CRTL_HOME_ACTIVE
))
{
cnt
++;
if (cnt
> 50) // erst nach Verzoegerung
{
// Erst mal initialisieren
cnt
= 0;
gps_tick
= 0;
hold_fast
= 0;
hold_reset_int
= 0; // Integrator enablen
int_east
= 0, int_north
= 0;
gps_reg_x
= 0, gps_reg_y
= 0;
delta_east
= 0, delta_north
= 0;
dist_flown
= 0;
gps_g2t_act_v
= 0;
gps_sub_state
= GPS_CRTL_IDLE
;
// aktuelle positionsdaten abspeichern
if (gps_rel_act_position.
status > 0)
{
gps_rel_start_position.
utm_east = gps_rel_act_position.
utm_east;
gps_rel_start_position.
utm_north= gps_rel_act_position.
utm_north;
gps_rel_start_position.
status = 1; // gueltige Positionsdaten
gps_rel_hold_position.
utm_east = gps_rel_act_position.
utm_east;
gps_rel_hold_position.
utm_north = gps_rel_act_position.
utm_north;
gps_rel_hold_position.
status = 1; // gueltige Positionsdaten
//Richtung zur Home Position bezogen auf Nordpol bestimmen
hdng_2home
= arctan_i
(-gps_rel_start_position.
utm_east,-gps_rel_start_position.
utm_north);
// in Winkel 0...360 Grad umrechnen
if (( gps_rel_start_position.
utm_east < 0)) hdng_2home
= ( 90-hdng_2home
);
else hdng_2home
= (270 - hdng_2home
);
dist_2home
= (int) get_dist
(gps_rel_start_position.
utm_east,gps_rel_start_position.
utm_north,hdng_2home
); //Entfernung zur Home Position bestimmen
gps_state
= GPS_CRTL_HOME_ACTIVE
;
return (GPS_STST_OK
);
}
else
{
gps_rel_start_position.
status = 0; //Keine Daten verfuegbar
gps_state
= GPS_CRTL_IDLE
;
return(GPS_STST_ERR
); // Keine Daten da
}
}
else return(GPS_STST_PEND
); // noch warten
}
break;
// ******************************
case GPS_CMD_REQ_HOLD
: // Die Lageregelung soll aktiviert werden.
if (gps_state
!= GPS_CRTL_HOLD_ACTIVE
)
{
cnt
++;
if (cnt
> 600) // erst nach Verzoegerung
{
cnt
= 0;
// aktuelle positionsdaten abspeichern
if (gps_rel_act_position.
status > 0)
{
hold_fast
= 0;
hold_reset_int
= 0; // Integrator enablen
int_east
= 0, int_north
= 0;
gps_reg_x
= 0, gps_reg_y
= 0;
delta_east
= 0, delta_north
= 0;
speed_east
= 0; speed_north
= 0;
int_ovfl_cnt
= 0;
gps_quiet_cnt
= 0;
gps_rel_hold_position.
utm_east = gps_rel_act_position.
utm_east;
gps_rel_hold_position.
utm_north = gps_rel_act_position.
utm_north;
gps_rel_hold_position.
status = 1; // gueltige Positionsdaten
gps_state
= GPS_CRTL_HOLD_ACTIVE
;
return (GPS_STST_OK
);
}
else
{
gps_rel_hold_position.
status = 0; //Keine Daten verfuegbar
gps_state
= GPS_CRTL_IDLE
;
return(GPS_STST_ERR
); // Keine Daten da
}
}
else return(GPS_STST_PEND
); // noch warten
}
break;
case GPS_CMD_STOP
: // Lageregelung beenden
cnt
= 0;
GPS_Nick
= 0;
GPS_Roll
= 0;
gps_sub_state
= GPS_CRTL_IDLE
;
gps_state
= GPS_CRTL_IDLE
;
return (GPS_STST_OK
);
break;
default:
return (GPS_STST_ERR
);
break;
}
switch (gps_state
)
{
case GPS_CRTL_IDLE
:
cnt
= 0;
return (GPS_STST_OK
);
break;
case GPS_CRTL_HOME_ACTIVE
: // Rueckflug zur Basis
//Der Sollwert des Lagereglers wird der Homeposition angenaehert
if (gps_rel_start_position.
status >0)
{
if ((gps_updte_flag
> 0) && (gps_sub_state
!=GPS_HOME_FINISHED
)) // nur wenn neue GPS Daten vorliegen und nicht schon alles fertig ist
{
gps_tick
++;
int d1
,d2
,d3
;
d1
= abs (gps_rel_hold_position.
utm_east - gps_rel_act_position.
utm_east );
d2
= abs (gps_rel_hold_position.
utm_north - gps_rel_act_position.
utm_north );
d3
= (dist_2home
- dist_flown
); // Restdistanz zum Ziel
if (d3
> GPS_G2T_DIST_MAX_STOP
) // Schneller Rueckflug, noch weit weg vom Ziel
{
if ((d1
< GPS_G2T_FAST_TOL
) && (d2
< GPS_G2T_FAST_TOL
)) //nur weiter wenn Lage innerhalb der Toleranz
{
if (gps_g2t_act_v
< GPS_G2T_V_MAX
-3) gps_g2t_act_v
+= 4; //Geschwindigkeit erhoehen
dist_flown
+=gps_g2t_act_v
; // Vorgabe der Strecke anhand der Geschwindigkeit
gps_sub_state
= GPS_HOME_FAST_IN_TOL
;
}
else //Den Lageregler in Ruhe arbeiten lassen weil ausserhalb der Toleranz
{
if (gps_g2t_act_v
> 1) gps_g2t_act_v
--; // Geschwindigkeit reduzieren
// dist_flown++; //Auch ausserhalb der Toleranz langsam erhoehen
gps_sub_state
= GPS_HOME_FAST_OUTOF_TOL
;
}
hold_reset_int
= 0; // Integrator einsschalten
hold_fast
= 1; // Regler fuer schnellen Flug
dist_frm_start_east
= (int)(((long)dist_flown
* (long)sin_i
(hdng_2home
))/1000);
dist_frm_start_north
= (int)(((long)dist_flown
* (long)cos_i
(hdng_2home
))/1000);
gps_rel_hold_position.
utm_east = gps_rel_start_position.
utm_east + dist_frm_start_east
; //naechster Zielpunkt
gps_rel_hold_position.
utm_north = gps_rel_start_position.
utm_north + dist_frm_start_north
; //naechster Zielpunkt
}
else if (d3
> GPS_G2T_DIST_HOLD
) //Das Ziel naehert sich, deswegen abbremsen
{
if ((d1
< GPS_G2T_NRML_TOL
) && (d2
< GPS_G2T_NRML_TOL
))
{
dist_flown
+= GPS_G2T_V_RAMP_DWN
; // Vorgabe der Strecke anhand der Geschwindigkeit
gps_sub_state
= GPS_HOME_RMPDWN_IN_TOL
;
}
else
{
dist_flown
++; //Auch ausserhalb der Toleranz langsam erhoehen
gps_sub_state
= GPS_HOME_RMPDWN_OUTOF_TOL
;
}
hold_reset_int
= 0; // Integrator einsschalten
hold_fast
= 1; // Regler fuer schnellen Flug
dist_frm_start_east
= (int)(((long)dist_flown
* (long)sin_i
(hdng_2home
))/1000);
dist_frm_start_north
= (int)(((long)dist_flown
* (long)cos_i
(hdng_2home
))/1000);
gps_rel_hold_position.
utm_east = gps_rel_start_position.
utm_east + dist_frm_start_east
; //naechster Zielpunkt
gps_rel_hold_position.
utm_north = gps_rel_start_position.
utm_north + dist_frm_start_north
; //naechster Zielpunkt
}
else //Soll-Ziel fast erreicht, Jetzt noch Reste ausgleichen, weil Zielpunkt nicht exakt bestimmt werden konnte (Fehler in Winkelfkt)
{
if ((d1
< GPS_G2T_NRML_TOL
) && (d2
< GPS_G2T_NRML_TOL
)) // Jetzt bis zum Zielpunkt regeln
{
gps_sub_state
= GPS_HOME_IN_TOL
;
hold_fast
= 0; // Wieder normal regeln
hold_reset_int
= 0; // Integrator einsschalten
if (gps_rel_hold_position.
utm_east >= GPS_G2T_V_MIN
) gps_rel_hold_position.
utm_east -= GPS_G2T_V_MIN
;
else if (gps_rel_hold_position.
utm_east <= -GPS_G2T_V_MIN
) gps_rel_hold_position.
utm_east += GPS_G2T_V_MIN
;
if (gps_rel_hold_position.
utm_north >= GPS_G2T_V_MIN
) gps_rel_hold_position.
utm_north -= GPS_G2T_V_MIN
;
else if (gps_rel_hold_position.
utm_north <= - GPS_G2T_V_MIN
) gps_rel_hold_position.
utm_north += GPS_G2T_V_MIN
;
if ((abs(gps_rel_hold_position.
utm_east) <= GPS_G2T_V_MIN
) && (abs(gps_rel_hold_position.
utm_north) <=GPS_G2T_V_MIN
))
{
gps_rel_hold_position.
utm_east = 0;
gps_rel_hold_position.
utm_north = 0;
gps_sub_state
= GPS_HOME_FINISHED
;
}
}
else gps_sub_state
= GPS_HOME_OUTOF_TOL
;
}
}
gps_state
= GPS_CRTL_HOLD_ACTIVE
; //Zwischensprung
return (GPS_STST_OK
);
}
else // Keine GPS Daten verfuegbar, deswegen Abbruch
{
gps_state
= GPS_CRTL_IDLE
;
return (GPS_STST_ERR
);
}
break;
case GPS_CRTL_HOLD_ACTIVE
: // Hier werden die Daten fuer Nick und Roll errechnet
if (gps_updte_flag
>0) // nur wenn neue GPS Daten vorliegen
{
gps_quiet_cnt
++;
// ab hier wird geregelt
delta_east
= (long) (gps_rel_act_position.
utm_east - gps_rel_hold_position.
utm_east);
delta_north
= (long) (gps_rel_act_position.
utm_north - gps_rel_hold_position.
utm_north);
int_east
+= (int)delta_east
;
int_north
+= (int)delta_north
;
speed_east
= actual_speed.
speed_e;
speed_north
= actual_speed.
speed_n;
gps_updte_flag
= 0; // Neue Werte koennen vom GPS geholt werden
dist_east
= (int)delta_east
; //merken
dist_north
= (int)delta_north
;
#define GPSINT_MAX 3000 // Neues Verfahren ab 30.12.2007 bei Integratoroverflow
if ((abs(int_east
) > GPSINT_MAX
) || (abs(int_north
)> GPSINT_MAX
))
{
if (int_ovfl_cnt
< 40) int_ovfl_cnt
+= 1; // Zahl der Overflows zaehlen
}
if (int_ovfl_cnt
> 0) //bei Overflow Wert Integratorwert reduzieren
{
int_ovfl_cnt
-= 1;
int_east
= (int_east
*7)/8; // Wert reduzieren
int_north
= (int_north
*7)/8;
}
if (hold_reset_int
> 0) //Im Schnellen Mode Integrator abschalten
{
int_east
= 0;
int_north
= 0;
}
//I Werte begrenzen
#define INT1_MAX (GPS_NICKROLL_MAX * GPS_V*3)/10// auf 30 Prozent des maximalen Nick/Rollwert begrenzen
int_east1
= ((((long)int_east
) * Parameter_UserParam2
)/32)/GPS_USR_PAR_FKT
;
int_north1
= ((((long)int_north
) * Parameter_UserParam2
)/32)/GPS_USR_PAR_FKT
;
if (int_east1
> INT1_MAX
) int_east1
= INT1_MAX
; //begrenzen
else if (int_east1
< -INT1_MAX
) int_east1
= -INT1_MAX
;
if (int_north1
> INT1_MAX
) int_north1
= INT1_MAX
; //begrenzen
else if (int_north1
< -INT1_MAX
) int_north1
= -INT1_MAX
;
if (hold_fast
> 0) //schneller Coming Home Modus
{
amplfy_speed_east
= DIFF_Y_F_MAX
;
amplfy_speed_north
= DIFF_Y_F_MAX
;
amplfy_speed_east
*= (Parameter_UserParam3
/GPS_USR_PAR_FKT
);
amplfy_speed_north
*= (Parameter_UserParam3
/GPS_USR_PAR_FKT
);
// speed_east = (speed_east * abs(speed_east) * (long)amplfy_speed_east ) /40000; //quadrieren
// speed_north = (speed_north * abs(speed_north) * (long)amplfy_speed_north) /40000; //quadrieren
speed_east
= (speed_east
* (long)amplfy_speed_east
) /100;
speed_north
= (speed_north
* (long)amplfy_speed_north
)/100;
// D Werte begrenzen
#define D_F_MAX (GPS_NICKROLL_MAX * GPS_V*7)/10 // auf xx Prozent des Maximalen Nick/Rollwert begrenzen
if (speed_east
> D_F_MAX
) speed_east
= D_F_MAX
;
else if (speed_east
< -D_F_MAX
) speed_east
= -D_F_MAX
;
if (speed_north
> D_F_MAX
) speed_north
= D_F_MAX
;
else if (speed_north
< -D_F_MAX
) speed_north
= -D_F_MAX
;
diff_p
= (Parameter_UserParam1
* GPS_PROP_FAST_V
)/GPS_USR_PAR_FKT
; //Verstaerkung fuer P-Anteil
}
else //langsamer Holdmodus
{
amplfy_speed_east
= DIFF_Y_N_MAX
;
amplfy_speed_north
= DIFF_Y_N_MAX
;
amplfy_speed_east
*= (Parameter_UserParam3
/GPS_USR_PAR_FKT
);
amplfy_speed_north
*= (Parameter_UserParam3
/GPS_USR_PAR_FKT
);
// speed_east = (speed_east * abs(speed_east) * (long)amplfy_speed_east) /20000; //quadrieren
// speed_north = (speed_north * abs(speed_north) * (long)amplfy_speed_north) /20000; //quadrieren
speed_east
= (speed_east
* (long)amplfy_speed_east
) /50;
speed_north
= (speed_north
* (long)amplfy_speed_north
)/50;
// D Werte begrenzen
#define D_N_MAX (GPS_NICKROLL_MAX * GPS_V*7)/10 // auf xx Prozent des Maximalen Nick/Rollwert begrenzen
if (speed_east
> D_N_MAX
) speed_east
= D_N_MAX
;
else if (speed_east
< -D_N_MAX
) speed_east
= -D_N_MAX
;
if (speed_north
> D_N_MAX
) speed_north
= D_N_MAX
;
else if (speed_north
< -D_N_MAX
) speed_north
= -D_N_MAX
;
diff_p
= (Parameter_UserParam1
* GPS_PROP_NRML_V
)/GPS_USR_PAR_FKT
; //Verstaerkung fuer P-Anteil
}
debug_gp_4
= (int)speed_east
; // zum Debuggen
debug_gp_5
= (int)speed_north
; // zum Debuggen
//P-Werte quadrieren
// delta_east = (abs(delta_east) * delta_east )/20; //quadrieren
// delta_north = (abs(delta_north) * delta_north)/20; //quadrieren
// delta_east = (delta_east )/2; //quadrieren
// delta_north = (delta_north)/2; //quadrieren
delta_east
= (delta_east
* (long)diff_p
)/(20);
delta_north
= (delta_north
* (long)diff_p
)/(20);
if (hold_fast
> 0) //schneller Coming Home Modus
{
// P Werte begrenzen
#define P1_F_MAX (GPS_NICKROLL_MAX * GPS_V*5)/10 // auf xx Prozent des Maximalen Nick/Rollwert begrenzen
if (delta_east
> P1_F_MAX
) delta_east
= P1_F_MAX
;
else if (delta_east
< -P1_F_MAX
) delta_east
= -P1_F_MAX
;
if (delta_north
> P1_F_MAX
) delta_north
= P1_F_MAX
;
else if (delta_north
< -P1_F_MAX
) delta_north
= -P1_F_MAX
;
}
else // Hold modus
{
// P Werte begrenzen
#define P1_N_MAX (GPS_NICKROLL_MAX * GPS_V*5)/10 // auf xx Prozent des Maximalen Nick/Rollwert begrenzen
if (delta_east
> P1_N_MAX
) delta_east
= P1_N_MAX
;
else if (delta_east
< -P1_N_MAX
) delta_east
= -P1_N_MAX
;
if (delta_north
> P1_N_MAX
) delta_north
= P1_N_MAX
;
else if (delta_north
< -P1_N_MAX
) delta_north
= -P1_N_MAX
;
}
debug_gp_2
= (int)delta_east
; // zum Debuggen
debug_gp_3
= (int)delta_north
; // zum Debuggen
//PID Regler Werte aufsummieren
gps_reg_x
= -(int_east1
+ delta_east
+ speed_east
); // I + P +D Anteil X Achse
gps_reg_y
= -(int_north1
+ delta_north
+ speed_north
); // I + P +D Anteil Y Achse
debug_gp_0
= (int)gps_reg_x
; // zum Debuggen
debug_gp_1
= (int)gps_reg_y
; // zum Debuggen
// Werte fuer Nick und Roll direkt aus gps_reg_x und gps_reg_y bestimmen
n
= GyroKomp_Int
/GYROKOMP_INC_GRAD_DEFAULT
; //Ausrichtung Kopter
ni
= -((gps_reg_y
* (long)cos_i
(n
)) + (gps_reg_x
* (long)sin_i
(n
)))/(1000*GPS_V
);
ro
= ((gps_reg_x
* (long)cos_i
(n
)) - (gps_reg_y
* (long)sin_i
(n
)))/(1000*GPS_V
);
if (ni
> (GPS_NICKROLL_MAX
)) ni
= (GPS_NICKROLL_MAX
);
else if (ni
< -(GPS_NICKROLL_MAX
)) ni
= -(GPS_NICKROLL_MAX
);
if (ro
> (GPS_NICKROLL_MAX
)) ro
= (GPS_NICKROLL_MAX
);
else if (ro
< -(GPS_NICKROLL_MAX
)) ro
= -(GPS_NICKROLL_MAX
);
if ((abs(dist_east
) > GPS_DIST_MAX
) || (abs(dist_north
) > GPS_DIST_MAX
)) // bei zu grossem Abstand abbrechen
{
GPS_Roll
= 0;
GPS_Nick
= 0;
gps_state
= GPS_CRTL_IDLE
;
return (GPS_STST_ERR
);
break;
}
else if ((PPM_in
[7] > 100) && (CAM_GPS_QUIET
> 0) && (gps_quiet_cnt
<=4) ) // Wenn Fotoausloeser gedruckt wird, GPS Stellwerte kurzzeitig auf 0 setzen
{
gps_quiet_cnt
++;
GPS_Roll
= 0;
GPS_Nick
= 0;
if ( cmd
== GPS_CMD_REQ_HOME
) gps_state
= GPS_CRTL_HOME_ACTIVE
; // State umsetzen
return (GPS_STST_OK
);
}
else if ((PPM_in
[7] < 50) && (CAM_GPS_QUIET
> 0) && (gps_quiet_cnt
>= 4))
{
gps_quiet_cnt
= 0;
if ( cmd
== GPS_CMD_REQ_HOME
) gps_state
= GPS_CRTL_HOME_ACTIVE
; // State umsetzen
return (GPS_STST_OK
);
}
else
{
GPS_Roll
= (int)ro
;
GPS_Nick
= (int)ni
;
if ( cmd
== GPS_CMD_REQ_HOME
) gps_state
= GPS_CRTL_HOME_ACTIVE
; // State umsetzen
return (GPS_STST_OK
);
}
}
else
{
if ( cmd
== GPS_CMD_REQ_HOME
) gps_state
= GPS_CRTL_HOME_ACTIVE
; // State umsetzen
return (GPS_STST_OK
);
}
break;
default:
gps_state
= GPS_CRTL_IDLE
;
return (GPS_STST_ERR
);
break;
}
return (GPS_STST_ERR
);
}