add tcas functions for collision avoidance

This commit is contained in:
Gautier Hattenberger
2008-05-02 10:38:52 +00:00
parent a8caf894df
commit 6018796e5c
2 changed files with 215 additions and 0 deletions
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/*
* Paparazzi mcu0 $Id$
*
* Copyright (C) 2003-2005 Pascal Brisset, Antoine Drouin
*
* This file is part of paparazzi.
*
* paparazzi 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, or (at your option)
* any later version.
*
* paparazzi 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 paparazzi; see the file COPYING. If not, write to
* the Free Software Foundation, 59 Temple Place - Suite 330,
* Boston, MA 02111-1307, USA.
*
*/
/** \file tcas.c
* \brief Collision avoidance library
*
*/
#include "tcas.h"
#include "airframe.h"
#include "estimator.h"
#include "nav.h"
#include "gps.h"
#include "flight_plan.h"
float tcas_alt_setpoint;
float tcas_tau_ta, tcas_tau_ra, tcas_dmod, tcas_alim;
uint8_t tcas_status;
uint8_t tcas_ac_RA;
uint8_t tcas_acs_status[NB_ACS];
#ifndef TCAS_TAU_TA // Traffic Advisory
#define TCAS_TAU_TA 2*CARROT
#endif
#ifndef TCAS_TAU_RA // Resolution Advisory
#define TCAS_TAU_RA CARROT
#endif
#ifndef TCAS_DMOD // Distance Modification
#define TCAS_DMOD 10.
#endif
#ifndef TCAS_ALIM // Altitude Limit
#define TCAS_ALIM 10.
#endif
#ifndef TCAS_DT_MAX
#define TCAS_DT_MAX 1500 // ms
#endif
#define TCAS_HUGE_TAU 100*TCAS_TAU_TA
void tcas_init( void ) {
tcas_alt_setpoint = GROUND_ALT + SECURITY_HEIGHT;
tcas_tau_ta = TCAS_TAU_TA;
tcas_tau_ra = TCAS_TAU_RA;
tcas_dmod = TCAS_DMOD;
tcas_alim = TCAS_ALIM;
tcas_status = TCAS_NO_ALARM;
tcas_ac_RA = AC_ID;
uint8_t i;
for (i = 0; i < NB_ACS; i++) tcas_acs_status[i] = TCAS_NO_ALARM;
}
/* conflicts detection and monitoring */
void tcas_periodic_task_1Hz( void ) {
// test possible conflicts
float tau_min = tcas_tau_ta;
uint8_t ac_id_close = AC_ID;
uint8_t i;
float vx = estimator_hspeed_mod * sin(estimator_hspeed_dir);
float vy = estimator_hspeed_mod * cos(estimator_hspeed_dir);
for (i = 2; i < NB_ACS; i++) {
if (the_acs[i].ac_id == 0) continue; // no AC data
uint32_t dt = gps_itow - the_acs[i].itow;
if (dt > 3*TCAS_DT_MAX) {
tcas_acs_status[i] = TCAS_NO_ALARM; // timeout, reset status
continue;
}
if (dt > TCAS_DT_MAX) continue; // lost com but keep current status
float dx = the_acs[i].east - estimator_x;
float dy = the_acs[i].north - estimator_y;
float dz = the_acs[i].alt - estimator_z;
float dvx = vx - the_acs[i].gspeed * sin(the_acs[i].course);
float dvy = vy - the_acs[i].gspeed * cos(the_acs[i].course);
float dvz = estimator_z_dot - the_acs[i].climb;
float scal = (dvx*dx + dvy*dy + dvz*dz);
float tau = TCAS_HUGE_TAU;
if (scal > 0) tau = (dx*dx + dy*dy + dz*dz) / scal;
// monitor conflicts
switch (tcas_acs_status[i]) {
case TCAS_RA:
if (tau == TCAS_HUGE_TAU) tcas_acs_status[i] = TCAS_NO_ALARM; // conflict is now resolved
break;
case TCAS_TA:
if (tau < TCAS_TAU_RA) {
tcas_acs_status[i] = TCAS_RA; // TA -> RA
//TODO Downlink alert
break;
}
if (tau > TCAS_TAU_TA) tcas_acs_status[i] = TCAS_NO_ALARM; // conflict is now resolved
break;
case TCAS_NO_ALARM:
if (tau < TCAS_TAU_TA) {
tcas_acs_status[i] = TCAS_TA; // NO_ALARM -> TA
//TODO Downlink warning
}
if (tau < TCAS_TAU_RA) {
tcas_acs_status[i] = TCAS_RA; // NO_ALARM -> RA = big problem ?
//TODO Downlink alert
}
break;
}
// store closest AC
if (tau < tau_min) {
tau_min = tau;
ac_id_close = the_acs[i].ac_id;
}
}
// set current conflict mode
if (!(tcas_status == TCAS_RA && tcas_ac_RA != AC_ID && tcas_acs_status[the_acs_id[tcas_ac_RA]] == TCAS_RA)) {
tcas_status = tcas_acs_status[the_acs_id[ac_id_close]];
if (tcas_status == TCAS_RA) tcas_ac_RA = ac_id_close;
else tcas_ac_RA = AC_ID; // no conflicts
}
}
/* altitude control loop */
void tcas_periodic_task_4Hz( void ) {
// set alt setpoint
if (estimator_z > GROUND_ALT + SECURITY_HEIGHT) {
struct ac_info_ * ac = get_ac_info(tcas_ac_RA);
float dz = ac->alt - estimator_z;
if (dz > tcas_alim) // go up
tcas_alt_setpoint = Max(nav_altitude, ac->alt + tcas_alim);
if (dz < -tcas_alim) // go down
tcas_alt_setpoint = Min(nav_altitude, ac->alt - tcas_alim);
else // AC with the smallest ID goes down
{
if (AC_ID < tcas_ac_RA) tcas_alt_setpoint = Min(nav_altitude, ac->alt - tcas_alim);
else tcas_alt_setpoint = Max(nav_altitude, ac->alt + tcas_alim);
}
// Bound alt
tcas_alt_setpoint = Max(GROUND_ALT + SECURITY_HEIGHT, tcas_alt_setpoint);
}
else tcas_alt_setpoint = nav_altitude;
}
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/*
* Paparazzi mcu0 $Id$
*
* Copyright (C) 2003-2005 Pascal Brisset, Antoine Drouin
*
* This file is part of paparazzi.
*
* paparazzi 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, or (at your option)
* any later version.
*
* paparazzi 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 paparazzi; see the file COPYING. If not, write to
* the Free Software Foundation, 59 Temple Place - Suite 330,
* Boston, MA 02111-1307, USA.
*
*/
/** \file tcas.h
* \brief Collision avoidance library
*
*/
#ifndef TCAS_H
#define TCAS_H
#include "std.h"
#include "traffic_info.h"
extern float tcas_alt_setpoint;
extern float tcas_tau_ta, tcas_tau_ra, tcas_dmod, tcas_alim;
#define TCAS_NO_ALARM 0
#define TCAS_TA 1
#define TCAS_RA 2
extern uint8_t tcas_status;
extern uint8_t tcas_ac_RA;
extern uint8_t tcas_acs_status[NB_ACS];
extern void tcas_init( void );
extern void tcas_periodic_task_1Hz( void );
extern void tcas_periodic_task_4Hz( void );
#define CallTCAS() { if (tcas_status == TCAS_RA) v_ctl_altitude_setpoint = tcas_alt_setpoint; }
#endif // TCAS