Rename tools to ao-<foo>
[fw/altos] / aoview / aoview_state.c
diff --git a/aoview/aoview_state.c b/aoview/aoview_state.c
deleted file mode 100644 (file)
index 7efd33b..0000000
+++ /dev/null
@@ -1,349 +0,0 @@
-/*
- * Copyright © 2009 Keith Packard <keithp@keithp.com>
- *
- * 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; version 2 of the License.
- *
- * 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.
- */
-
-#include "aoview.h"
-#include <math.h>
-
-static inline double sqr(double a) { return a * a; };
-
-static void
-aoview_great_circle (double start_lat, double start_lon,
-                    double end_lat, double end_lon,
-                    double *dist, double *bearing)
-{
-       const double rad = M_PI / 180;
-       const double earth_radius = 6371.2 * 1000;      /* in meters */
-       double lat1 = rad * start_lat;
-       double lon1 = rad * -start_lon;
-       double lat2 = rad * end_lat;
-       double lon2 = rad * -end_lon;
-
-       double d_lat = lat2 - lat1;
-       double d_lon = lon2 - lon1;
-
-       /* From http://en.wikipedia.org/wiki/Great-circle_distance */
-       double vdn = sqrt(sqr(cos(lat2) * sin(d_lon)) +
-                         sqr(cos(lat1) * sin(lat2) -
-                             sin(lat1) * cos(lat2) * cos(d_lon)));
-       double vdd = sin(lat1) * sin(lat2) + cos(lat1) * cos(lat2) * cos(d_lon);
-       double d = atan2(vdn,vdd);
-       double course;
-
-       if (cos(lat1) < 1e-20) {
-               if (lat1 > 0)
-                       course = M_PI;
-               else
-                       course = -M_PI;
-       } else {
-               if (d < 1e-10)
-                       course = 0;
-               else
-                       course = acos((sin(lat2)-sin(lat1)*cos(d)) /
-                                     (sin(d)*cos(lat1)));
-               if (sin(lon2-lon1) > 0)
-                       course = 2 * M_PI-course;
-       }
-       *dist = d * earth_radius;
-       *bearing = course * 180/M_PI;
-}
-
-static void
-aoview_state_add_deg(int column, char *label, double deg, char pos, char neg)
-{
-       double  int_part;
-       double  min;
-       char    sign = pos;
-
-       if (deg < 0) {
-               deg = -deg;
-               sign = neg;
-       }
-       int_part = floor (deg);
-       min = (deg - int_part) * 60.0;
-       aoview_table_add_row(column, label, "%d°%lf'%c",
-                            (int) int_part, min, sign);
-
-}
-
-static char *ascent_states[] = {
-       "boost",
-       "fast",
-       "coast",
-       0,
-};
-
-static double
-aoview_time(void)
-{
-       struct timespec now;
-
-       clock_gettime(CLOCK_MONOTONIC, &now);
-       return (double) now.tv_sec + (double) now.tv_nsec / 1.0e9;
-}
-
-/*
- * Fill out the derived data fields
- */
-static void
-aoview_state_derive(struct aodata *data, struct aostate *state)
-{
-       int     i;
-       double  new_height;
-       double  height_change;
-       double  time_change;
-       int     tick_count;
-
-       state->report_time = aoview_time();
-
-       state->prev_data = state->data;
-       state->prev_npad = state->npad;
-       state->data = *data;
-       tick_count = data->tick;
-       if (tick_count < state->prev_data.tick)
-               tick_count += 65536;
-       time_change = (tick_count - state->prev_data.tick) / 100.0;
-
-       state->ground_altitude = aoview_pres_to_altitude(data->ground_pres);
-       new_height = aoview_pres_to_altitude(data->flight_pres) - state->ground_altitude;
-       height_change = new_height - state->height;
-       state->height = new_height;
-       if (time_change)
-               state->baro_speed = (state->baro_speed * 3 + (height_change / time_change)) / 4.0;
-       state->acceleration = (data->ground_accel - data->flight_accel) / 27.0;
-       state->speed = data->flight_vel / 2700.0;
-       state->temperature = ((data->temp / 32767.0 * 3.3) - 0.5) / 0.01;
-       state->drogue_sense = data->drogue / 32767.0 * 15.0;
-       state->main_sense = data->main / 32767.0 * 15.0;
-       state->battery = data->batt / 32767.0 * 5.0;
-       if (!strcmp(data->state, "pad")) {
-               if (data->gps.gps_locked && data->gps.nsat >= 4) {
-                       state->npad++;
-                       state->pad_lat_total += data->gps.lat;
-                       state->pad_lon_total += data->gps.lon;
-                       state->pad_alt_total += data->gps.alt;
-                       if (state->npad > 1) {
-                               state->pad_lat = (state->pad_lat * 31 + data->gps.lat) / 32.0;
-                               state->pad_lon = (state->pad_lon * 31 + data->gps.lon) / 32.0;
-                               state->pad_alt = (state->pad_alt * 31 + data->gps.alt) / 32.0;
-                       } else {
-                               state->pad_lat = data->gps.lat;
-                               state->pad_lon = data->gps.lon;
-                               state->pad_alt = data->gps.alt;
-                       }
-               }
-       }
-       state->ascent = FALSE;
-       for (i = 0; ascent_states[i]; i++)
-               if (!strcmp(data->state, ascent_states[i]))
-                       state->ascent = TRUE;
-
-       /* Only look at accelerometer data on the way up */
-       if (state->ascent && state->acceleration > state->max_acceleration)
-               state->max_acceleration = state->acceleration;
-       if (state->ascent && state->speed > state->max_speed)
-               state->max_speed = state->speed;
-
-       if (state->height > state->max_height)
-               state->max_height = state->height;
-       state->gps.gps_locked = data->gps.gps_locked;
-       state->gps.gps_connected = data->gps.gps_connected;
-       if (data->gps.gps_locked) {
-               state->gps = data->gps;
-               state->gps_valid = 1;
-               if (state->npad)
-                       aoview_great_circle(state->pad_lat, state->pad_lon, state->gps.lat, state->gps.lon,
-                                           &state->distance, &state->bearing);
-       }
-       if (state->npad) {
-               state->gps_height = state->gps.alt - state->pad_alt;
-       } else {
-               state->gps_height = 0;
-       }
-}
-
-void
-aoview_speak_state(struct aostate *state)
-{
-       if (strcmp(state->data.state, state->prev_data.state)) {
-               aoview_voice_speak("%s\n", state->data.state);
-               if (!strcmp(state->data.state, "drogue"))
-                       aoview_voice_speak("apogee %d meters\n",
-                                          (int) state->max_height);
-               if (!strcmp(state->prev_data.state, "boost"))
-                       aoview_voice_speak("max speed %d meters per second\n",
-                                          (int) state->max_speed);
-       }
-       if (state->prev_npad < MIN_PAD_SAMPLES && state->npad >= MIN_PAD_SAMPLES)
-               aoview_voice_speak("g p s ready\n");
-}
-
-void
-aoview_speak_height(struct aostate *state)
-{
-       aoview_voice_speak("%d meters\n", state->height);
-}
-
-struct aostate aostate;
-
-static guint aostate_timeout;
-
-#define COMPASS_LIMIT(n)       ((n * 22.5) + 22.5/2)
-
-static char *compass_points[] = {
-       "north",
-       "north north east",
-       "north east",
-       "east north east",
-       "east",
-       "east south east",
-       "south east",
-       "south south east",
-       "south",
-       "south south west",
-       "south west",
-       "west south west",
-       "west",
-       "west north west",
-       "north west",
-       "north north west",
-};
-
-static char *
-aoview_compass_point(double bearing)
-{
-       int     i;
-       while (bearing < 0)
-               bearing += 360.0;
-       while (bearing >= 360.0)
-               bearing -= 360.0;
-
-       i = floor ((bearing - 22.5/2) / 22.5 + 0.5);
-       if (i < 0) i = 0;
-       if (i >= sizeof (compass_points) / sizeof (compass_points[0]))
-               i = 0;
-       return compass_points[i];
-}
-
-static gboolean
-aoview_state_timeout(gpointer data)
-{
-       double  now = aoview_time();
-
-       if (strlen(aostate.data.state) > 0 && strcmp(aostate.data.state, "pad") != 0)
-               aoview_speak_height(&aostate);
-       if (now - aostate.report_time >= 20 || !strcmp(aostate.data.state, "landed")) {
-               if (!aostate.ascent) {
-                       if (fabs(aostate.baro_speed) < 20 && aostate.height < 100)
-                               aoview_voice_speak("rocket landed safely\n");
-                       else
-                               aoview_voice_speak("rocket may have crashed\n");
-                       if (aostate.gps_valid) {
-                               aoview_voice_speak("rocket reported %s of pad distance %d meters\n",
-                                                  aoview_compass_point(aostate.bearing),
-                                                  (int) aostate.distance);
-                       }
-               }
-               aostate_timeout = 0;
-               return FALSE;
-       }
-       return TRUE;
-}
-
-void
-aoview_state_reset(void)
-{
-       memset(&aostate, '\0', sizeof (aostate));
-}
-
-void
-aoview_state_notify(struct aodata *data)
-{
-       struct aostate *state = &aostate;
-       aoview_state_derive(data, state);
-       aoview_table_start();
-
-       if (state->npad >= MIN_PAD_SAMPLES)
-               aoview_table_add_row(0, "Ground state", "ready");
-       else
-               aoview_table_add_row(0, "Ground state", "waiting for gps (%d)",
-                                    MIN_PAD_SAMPLES - state->npad);
-       aoview_table_add_row(0, "Rocket state", "%s", state->data.state);
-       aoview_table_add_row(0, "Callsign", "%s", state->data.callsign);
-       aoview_table_add_row(0, "Rocket serial", "%d", state->data.serial);
-
-       aoview_table_add_row(0, "RSSI", "%6ddBm", state->data.rssi);
-       aoview_table_add_row(0, "Height", "%6dm", state->height);
-       aoview_table_add_row(0, "Max height", "%6dm", state->max_height);
-       aoview_table_add_row(0, "Acceleration", "%7.1fm/s²", state->acceleration);
-       aoview_table_add_row(0, "Max acceleration", "%7.1fm/s²", state->max_acceleration);
-       aoview_table_add_row(0, "Speed", "%7.1fm/s", state->ascent ? state->speed : state->baro_speed);
-       aoview_table_add_row(0, "Max Speed", "%7.1fm/s", state->max_speed);
-       aoview_table_add_row(0, "Temperature", "%6.2f°C", state->temperature);
-       aoview_table_add_row(0, "Battery", "%5.2fV", state->battery);
-       aoview_table_add_row(0, "Drogue", "%5.2fV", state->drogue_sense);
-       aoview_table_add_row(0, "Main", "%5.2fV", state->main_sense);
-       aoview_table_add_row(0, "Pad altitude", "%dm", state->ground_altitude);
-       aoview_table_add_row(1, "Satellites", "%d", state->gps.nsat);
-       if (state->gps.gps_locked) {
-               aoview_table_add_row(1, "GPS", "locked");
-       } else if (state->gps.gps_connected) {
-               aoview_table_add_row(1, "GPS", "unlocked");
-       } else {
-               aoview_table_add_row(1, "GPS", "not available");
-       }
-       if (state->gps_valid) {
-               aoview_state_add_deg(1, "Latitude", state->gps.lat, 'N', 'S');
-               aoview_state_add_deg(1, "Longitude", state->gps.lon, 'E', 'W');
-               aoview_table_add_row(1, "GPS height", "%d", state->gps_height);
-               aoview_table_add_row(1, "GPS time", "%02d:%02d:%02d",
-                                    state->gps.gps_time.hour,
-                                    state->gps.gps_time.minute,
-                                    state->gps.gps_time.second);
-       }
-       if (state->gps.gps_extended) {
-               aoview_table_add_row(1, "GPS ground speed", "%7.1fm/s %d°",
-                                    state->gps.ground_speed,
-                                    state->gps.course);
-               aoview_table_add_row(1, "GPS climb rate", "%7.1fm/s",
-                                    state->gps.climb_rate);
-               aoview_table_add_row(1, "GPS precision", "%4.1f(hdop) %3dm(h) %3dm(v)",
-                                    state->gps.hdop, state->gps.h_error, state->gps.v_error);
-       }
-       if (state->npad) {
-               aoview_table_add_row(1, "Distance from pad", "%5.0fm", state->distance);
-               aoview_table_add_row(1, "Direction from pad", "%4.0f°", state->bearing);
-               aoview_state_add_deg(1, "Pad latitude", state->pad_lat, 'N', 'S');
-               aoview_state_add_deg(1, "Pad longitude", state->pad_lon, 'E', 'W');
-               aoview_table_add_row(1, "Pad GPS alt", "%gm", state->pad_alt);
-       }
-       aoview_table_finish();
-       aoview_label_show(state);
-       aoview_speak_state(state);
-       if (!aostate_timeout && strcmp(state->data.state, "pad") != 0)
-               aostate_timeout = g_timeout_add_seconds(10, aoview_state_timeout, NULL);
-}
-
-void
-aoview_state_new(void)
-{
-}
-
-void
-aoview_state_init(GladeXML *xml)
-{
-       aoview_state_new();
-}