ao-tools: Add lots of compiler warning flags to ao-tools build
[fw/altos] / ao-tools / ao-postflight / ao-postflight.c
index 4ca39c2448a2483359643776afecede920655dea..e5b556652b934be857a24f6da7d7b72999f72f1f 100644 (file)
@@ -39,9 +39,32 @@ static const char *state_names[] = {
        "invalid"
 };
 
+static const char *kml_state_colours[] = {
+       "FF000000",
+       "FF000000",
+       "FF000000",
+       "FF0000FF",
+       "FF4080FF",
+       "FF00FFFF",
+       "FFFF0000",
+       "FF00FF00",
+       "FF000000",
+       "FFFFFFFF"
+};
+
+static int plot_colors[3][3] = {
+       { 0, 0x90, 0 }, /* height */
+       { 0xa0, 0, 0 }, /* speed */
+       { 0, 0, 0xc0 }, /* accel */
+};
+
+#define PLOT_HEIGHT    0
+#define PLOT_SPEED     1
+#define PLOT_ACCEL     2
+
 static void
 plot_perioddata(struct cc_perioddata *d, char *axis_label, char *plot_label,
-               double min_time, double max_time)
+               double min_time, double max_time, int plot_type)
 {
        double  *times;
        double  ymin, ymax;
@@ -60,11 +83,61 @@ plot_perioddata(struct cc_perioddata *d, char *axis_label, char *plot_label,
        ymax_i = cc_perioddata_max(d, min_time, max_time);
        ymin = d->data[ymin_i];
        ymax = d->data[ymax_i];
+       plscol0(1, 0, 0, 0);
+       plscol0(2, plot_colors[plot_type][0],  plot_colors[plot_type][1],  plot_colors[plot_type][2]);
+       plcol0(1);
        plenv(times[0], times[stop-start],
              ymin, ymax, 0, 2);
-       plcol0(1);
        pllab("Time", axis_label, plot_label);
+       plcol0(2);
        plline(stop - start + 1, times, d->data + start);
+       free(times);
+}
+
+static void
+plot_timedata(struct cc_timedata *d, char *axis_label, char *plot_label,
+             double min_time, double max_time, int plot_type)
+{
+       double  *times;
+       double  *values;
+       double  ymin, ymax;
+       int     ymin_i, ymax_i;
+       int     i;
+       int     start = -1, stop = -1;
+       double  start_time = 0, stop_time = 0;
+       int     num;
+
+       for (i = 0; i < d->num; i++) {
+               if (start < 0 && d->data[i].time >= min_time) {
+                       start_time = d->data[i].time;
+                       start = i;
+               }
+               if (d->data[i].time <= max_time) {
+                       stop_time = d->data[i].time;
+                       stop = i;
+               }
+       }
+
+       times = calloc(stop - start + 1, sizeof (double));
+       values = calloc(stop - start + 1, sizeof (double));
+
+       ymin_i = cc_timedata_min(d, min_time, max_time);
+       ymax_i = cc_timedata_max(d, min_time, max_time);
+       ymin = d->data[ymin_i].value;
+       ymax = d->data[ymax_i].value;
+       for (i = start; i <= stop; i++) {
+               times[i-start] = (d->data[i].time - start_time)/100.0;
+               values[i-start] = d->data[i].value;
+       }
+       plscol0(1, 0, 0, 0);
+       plscol0(2, plot_colors[plot_type][0],  plot_colors[plot_type][1],  plot_colors[plot_type][2]);
+       plcol0(1);
+       plenv(times[0], times[stop-start], ymin, ymax, 0, 2);
+       pllab("Time", axis_label, plot_label);
+       plcol0(2);
+       plline(stop - start + 1, times, values);
+       free(times);
+       free(values);
 }
 
 static struct cc_perioddata *
@@ -101,8 +174,122 @@ merge_data(struct cc_perioddata *first, struct cc_perioddata *last, double split
        return pd;
 }
 
+static const char kml_header_start[] =
+       "<?xml version=\"1.0\" encoding=\"UTF-8\"?>\n"
+       "<kml xmlns=\"http://www.opengis.net/kml/2.2\">\n"
+       "<Document>\n"
+       "  <name>%s</name>\n"
+       "  <description>\n";
+static const char kml_header_end[] =
+       "  </description>\n"
+       "  <open>0</open>\n";
+
+static const char kml_style_start[] =
+       "  <Style id=\"ao-flightstate-%s\">\n"
+       "    <LineStyle><color>%s</color><width>4</width></LineStyle>\n"
+       "    <BalloonStyle>\n"
+       "      <text>\n";
+static const char kml_style_end[] =
+       "      </text>\n"
+       "    </BalloonStyle>\n"
+       "  </Style>\n";
+
+static const char kml_placemark_start[] =
+       "  <Placemark>\n"
+       "    <name>%s</name>\n"
+       "    <styleUrl>#ao-flightstate-%s</styleUrl>\n"
+       "    <LineString>\n"
+       "      <tessellate>1</tessellate>\n"
+       "      <altitudeMode>absolute</altitudeMode>\n"
+       "      <coordinates>\n";
+
+static const char kml_coord_fmt[] =
+       "        %12.7f, %12.7f, %12.7f <!-- alt %12.7f time %12.7f sats %d -->\n";
+
+static const char kml_placemark_end[] =
+       "      </coordinates>\n"
+       "    </LineString>\n"
+       "  </Placemark>\n";
+
+static const char kml_footer[] =
+       "      </coordinates>\n"
+       "    </LineString>\n"
+       "  </Placemark>\n"
+       "</Document>\n"
+       "</kml>\n";
+
+static unsigned
+gps_daytime(struct cc_gpselt *gps)
+{
+       return ((gps->hour * 60 +
+                gps->minute) * 60 +
+               gps->second) * 1000;
+}
+
+int
+daytime_hour(unsigned daytime)
+{
+       return daytime / 1000 / 60 / 60;
+}
+
+int
+daytime_minute(unsigned daytime)
+{
+       return (daytime / 1000 / 60) % 60;
+}
+
+int
+daytime_second(unsigned daytime)
+{
+       return (daytime / 1000) % 60;
+}
+
+int
+daytime_millisecond(unsigned daytime)
+{
+       return daytime % 1000;
+}
+
+static unsigned
+compute_daytime_ms(double time, struct cc_gpsdata *gps)
+{
+       int     i;
+       unsigned        gps_start_daytime, gps_stop_daytime;
+
+       if (time <= gps->data[0].time) {
+               gps_stop_daytime = gps_daytime(&gps->data[0]);
+               return gps_stop_daytime - (gps->data[0].time - time) * 10;
+       }
+       for (i = 0; i < gps->num - 1; i++)
+               if (time > gps->data[i].time)
+                       break;
+       gps_start_daytime = gps_daytime(&gps->data[i]);
+       if (i == gps->num - 1) {
+               return gps_start_daytime + (time - gps->data[i].time) * 10;
+       } else {
+               unsigned        gps_period_daytime;
+               double          gps_period_time;
+               double          time_since_start;
+
+               gps_stop_daytime = gps_daytime(&gps->data[i + 1]);
+
+               /* range of gps daytime values */
+               gps_period_daytime = gps_stop_daytime - gps_start_daytime;
+
+               /* range of gps time values */
+               gps_period_time = gps->data[i+1].time - gps->data[i].time;
+
+               /* sample time after first gps time */
+               time_since_start = time - gps->data[i].time;
+
+               return gps_start_daytime +
+                       gps_period_daytime * time_since_start / gps_period_time;
+       }
+}
+
 static void
-analyse_flight(struct cc_flightraw *f, FILE *summary_file, FILE *detail_file, char *plot_name)
+analyse_flight(struct cc_flightraw *f, FILE *summary_file, FILE *detail_file,
+              FILE *raw_file, char *plot_name, FILE *gps_file, FILE *kml_file)
 {
        double  height;
        double  accel;
@@ -118,9 +305,34 @@ analyse_flight(struct cc_flightraw *f, FILE *summary_file, FILE *detail_file, ch
        double  state_start, state_stop;
        struct cc_flightcooked *cooked;
        double  apogee;
+       char    buf[128];
+
+       if (kml_file) {
+                snprintf(buf, sizeof (buf), "AO Flight#%d S/N: %03d", f->flight, f->serial);
+               fprintf(kml_file, kml_header_start, buf);
+       }
+
+       fprintf(summary_file,
+               "Serial:  %9d\n"
+               "Flight:  %9d\n",
+               f->serial, f->flight);
 
-       fprintf(summary_file, "Flight:  %9d\nSerial:  %9d\n",
-               f->flight, f->serial);
+       if (f->year) {
+               snprintf(buf, sizeof (buf),
+                       "Date:   %04d-%02d-%02d\n",
+                       f->year, f->month, f->day);
+               fprintf(summary_file, "%s", buf);
+               if (kml_file) fprintf(kml_file, "%s", buf);
+       }
+       if (f->gps.num) {
+               snprintf(buf, sizeof (buf),
+                       "Time:     %2d:%02d:%02d\n",
+                       f->gps.data[0].hour,
+                       f->gps.data[0].minute,
+                       f->gps.data[0].second);
+               fprintf(summary_file, "%s", buf);
+               if (kml_file) fprintf(kml_file, "%s", buf);
+       }
        boost_start = f->accel.data[0].time;
        boost_stop = f->accel.data[f->accel.num-1].time;
        for (i = 0; i < f->state.num; i++) {
@@ -141,10 +353,12 @@ analyse_flight(struct cc_flightraw *f, FILE *summary_file, FILE *detail_file, ch
                min_pres = f->pres.data[pres_i].value;
                height = cc_barometer_to_altitude(min_pres) -
                        cc_barometer_to_altitude(f->ground_pres);
-               fprintf(summary_file, "Max height: %9.2fm    %9.2fft   %9.2fs\n",
+               apogee = f->pres.data[pres_i].time;
+               snprintf(buf, sizeof (buf), "Max height: %9.2fm    %9.2fft   %9.2fs\n",
                        height, height * 100 / 2.54 / 12,
                        (f->pres.data[pres_i].time - boost_start) / 100.0);
-               apogee = f->pres.data[pres_i].time;
+               fprintf(summary_file, "%s", buf);
+               if (kml_file) fprintf(kml_file, "%s", buf);
        }
 
        cooked = cc_flight_cook(f);
@@ -152,9 +366,11 @@ analyse_flight(struct cc_flightraw *f, FILE *summary_file, FILE *detail_file, ch
                speed_i = cc_perioddata_max(&cooked->accel_speed, boost_start, boost_stop);
                if (speed_i >= 0) {
                        speed = cooked->accel_speed.data[speed_i];
-                       fprintf(summary_file, "Max speed:  %9.2fm/s  %9.2fft/s %9.2fs\n",
+                       snprintf(buf, sizeof (buf), "Max speed:  %9.2fm/s  %9.2fft/s %9.2fs\n",
                               speed, speed * 100 / 2.4 / 12.0,
                               (cooked->accel_speed.start + speed_i * cooked->accel_speed.step - boost_start) / 100.0);
+                       fprintf(summary_file, "%s", buf);
+                       if (kml_file) fprintf(kml_file, "%s", buf);
                }
        }
        accel_i = cc_timedata_min(&f->accel, boost_start, boost_stop);
@@ -162,11 +378,16 @@ analyse_flight(struct cc_flightraw *f, FILE *summary_file, FILE *detail_file, ch
        {
                accel = cc_accelerometer_to_acceleration(f->accel.data[accel_i].value,
                                                         f->ground_accel);
-               fprintf(summary_file, "Max accel:  %9.2fm/s² %9.2fg    %9.2fs\n",
+               snprintf(buf, sizeof (buf), "Max accel:  %9.2fm/s² %9.2fg    %9.2fs\n",
                        accel, accel /  9.80665,
                        (f->accel.data[accel_i].time - boost_start) / 100.0);
+               fprintf(summary_file, "%s", buf);
+               if (kml_file) fprintf(kml_file, "%s", buf);
        }
 
+       if (kml_file)
+               fprintf(kml_file, "%s", kml_header_end);
+
        for (i = 0; i < f->state.num; i++) {
                state = f->state.data[i].value;
                state_start = f->state.data[i].time;
@@ -179,14 +400,23 @@ analyse_flight(struct cc_flightraw *f, FILE *summary_file, FILE *detail_file, ch
                fprintf(summary_file, "State: %s\n", state_names[state]);
                fprintf(summary_file, "\tStart:      %9.2fs\n", (state_start - boost_start) / 100.0);
                fprintf(summary_file, "\tDuration:   %9.2fs\n", (state_stop - state_start) / 100.0);
+               if (kml_file) {
+                       fprintf(kml_file, kml_style_start, state_names[state], kml_state_colours[state]);
+                       fprintf(kml_file, "\tState: %s\n", state_names[state]);
+                       fprintf(kml_file, "\tStart:      %9.2fs\n", (state_start - boost_start) / 100.0);
+                       fprintf(kml_file, "\tDuration:   %9.2fs\n", (state_stop - state_start) / 100.0);
+               }
+
                accel_i = cc_timedata_min(&f->accel, state_start, state_stop);
                if (accel_i >= 0)
                {
                        accel = cc_accelerometer_to_acceleration(f->accel.data[accel_i].value,
                                                                 f->ground_accel);
-                       fprintf(summary_file, "\tMax accel:  %9.2fm/s² %9.2fg    %9.2fs\n",
+                       snprintf(buf, sizeof (buf), "\tMax accel:  %9.2fm/s² %9.2fg    %9.2fs\n",
                               accel, accel / 9.80665,
                               (f->accel.data[accel_i].time - boost_start) / 100.0);
+                       fprintf(summary_file, "%s", buf);
+                       if (kml_file) fprintf(kml_file, "%s", buf);
                }
 
                if (cooked) {
@@ -203,11 +433,16 @@ analyse_flight(struct cc_flightraw *f, FILE *summary_file, FILE *detail_file, ch
                        }
                        if (speed_i >= 0)
                        {
-                               fprintf(summary_file, "\tMax speed:  %9.2fm/s  %9.2fft/s %9.2fs\n",
+                               snprintf(buf, sizeof (buf), "\tMax speed:  %9.2fm/s  %9.2fft/s %9.2fs\n",
                                       speed, speed * 100 / 2.4 / 12.0,
                                       (cooked->accel_speed.start + speed_i * cooked->accel_speed.step - boost_start) / 100.0);
-                               fprintf(summary_file, "\tAvg speed:  %9.2fm/s  %9.2fft/s\n",
+                               fprintf(summary_file, "%s", buf);
+                               if (kml_file) fprintf(kml_file, "%s", buf);
+
+                               snprintf(buf, sizeof (buf), "\tAvg speed:  %9.2fm/s  %9.2fft/s\n",
                                        avg_speed, avg_speed * 100 / 2.4 / 12.0);
+                               fprintf(summary_file, "%s", buf);
+                               if (kml_file) fprintf(kml_file, "%s", buf);
                        }
                }
                pres_i = cc_timedata_min(&f->pres, state_start, state_stop);
@@ -216,30 +451,157 @@ analyse_flight(struct cc_flightraw *f, FILE *summary_file, FILE *detail_file, ch
                        min_pres = f->pres.data[pres_i].value;
                        height = cc_barometer_to_altitude(min_pres) -
                                cc_barometer_to_altitude(f->ground_pres);
-                       fprintf(summary_file, "\tMax height: %9.2fm    %9.2fft   %9.2fs\n",
+                       snprintf(buf, sizeof (buf), "\tMax height: %9.2fm    %9.2fft   %9.2fs\n",
                                height, height * 100 / 2.54 / 12,
                                (f->pres.data[pres_i].time - boost_start) / 100.0);
+                       fprintf(summary_file, "%s", buf);
+                       if (kml_file) fprintf(kml_file, "%s", buf);
                }
+               if (kml_file) fprintf(kml_file, "%s", kml_style_end);
        }
        if (cooked && detail_file) {
                double  max_height = 0;
                int     i;
                double  *times;
 
-               fprintf(detail_file, "%9s %9s %9s %9s\n",
-                      "time", "height", "speed", "accel");
+               fprintf(detail_file, "%9s %9s %9s %9s %9s\n",
+                       "time", "height", "speed", "accel", "daytime");
                for (i = 0; i < cooked->pres_pos.num; i++) {
-                       double  time = (cooked->accel_accel.start + i * cooked->accel_accel.step - boost_start) / 100.0;
+                       double  clock_time = cooked->accel_accel.start + i * cooked->accel_accel.step;
+                       double  time = (clock_time - boost_start) / 100.0;
                        double  accel = cooked->accel_accel.data[i];
                        double  pos = cooked->pres_pos.data[i];
                        double  speed;
+                       unsigned        daytime;
                        if (cooked->pres_pos.start + cooked->pres_pos.step * i < apogee)
                                speed = cooked->accel_speed.data[i];
                        else
                                speed = cooked->pres_speed.data[i];
-                       fprintf(detail_file, "%9.2f %9.2f %9.2f %9.2f\n",
-                              time, pos, speed, accel);
+                       if (f->gps.num)
+                               daytime = compute_daytime_ms(clock_time, &f->gps);
+                       else
+                               daytime = 0;
+                       fprintf(detail_file, "%9.2f %9.2f %9.2f %9.2f %02d:%02d:%02d.%03d\n",
+                               time, pos, speed, accel,
+                               daytime_hour(daytime),
+                               daytime_minute(daytime),
+                               daytime_second(daytime),
+                               daytime_millisecond(daytime));
+               }
+       }
+       if (raw_file) {
+               fprintf(raw_file, "%9s %9s %9s %9s\n",
+                       "time", "height", "accel", "daytime");
+               for (i = 0; i < cooked->pres.num; i++) {
+                       double time = cooked->pres.data[i].time;
+                       double pres = cooked->pres.data[i].value;
+                       double accel = cooked->accel.data[i].value;
+                       unsigned        daytime;
+                       if (f->gps.num)
+                               daytime = compute_daytime_ms(time, &f->gps);
+                       else
+                               daytime = 0;
+                       fprintf(raw_file, "%9.2f %9.2f %9.2f %02d:%02d:%02d.%03d\n",
+                               time, pres, accel,
+                               daytime_hour(daytime),
+                               daytime_minute(daytime),
+                               daytime_second(daytime),
+                               daytime_millisecond(daytime));
+               }
+       }
+       if (gps_file || kml_file) {
+               int     j = 0, baro_pos;
+               double  baro_offset;
+               double  baro = 0.0;
+               int     state_idx = 0;
+
+               if (gps_file)
+                       fprintf(gps_file, "%2s %2s %2s %9s %12s %12s %9s %8s %5s\n",
+                               "hr", "mn", "sc",
+                               "time", "lat", "lon", "alt", "baro", "nsat");
+               if (kml_file)
+                       fprintf(kml_file, kml_placemark_start,
+                               state_names[(int)f->state.data[state_idx].value],
+                               state_names[(int)f->state.data[state_idx].value]); 
+
+               if (f->gps.num)
+                       baro_offset = f->gps.data[0].alt;
+               else
+                       baro_offset = 0;
+               baro_pos = 0;
+               for (i = 0; i < f->gps.num; i++) {
+                       int     nsat = 0;
+                       int     k;
+                       while (j < f->gps.numsats - 1) {
+                               if (f->gps.sats[j].sat[0].time <= f->gps.data[i].time &&
+                                   f->gps.data[i].time < f->gps.sats[j+1].sat[0].time)
+                                       break;
+                               j++;
+                       }
+                       if (cooked) {
+                               while (baro_pos < cooked->pres_pos.num) {
+                                       double  baro_time = cooked->accel_accel.start + baro_pos * cooked->accel_accel.step;
+                                       if (baro_time >= f->gps.data[i].time)
+                                               break;
+                                       baro_pos++;
+                               }
+                               if (baro_pos < cooked->pres_pos.num)
+                                       baro = cooked->pres_pos.data[baro_pos];
+                       }
+                       if (gps_file)
+                               fprintf(gps_file, "%2d %2d %2d %12.7f %12.7f %12.7f %7.1f %7.1f",
+                                       f->gps.data[i].hour,
+                                       f->gps.data[i].minute,
+                                       f->gps.data[i].second,
+                                       (f->gps.data[i].time - boost_start) / 100.0,
+                                       f->gps.data[i].lat,
+                                       f->gps.data[i].lon,
+                                       f->gps.data[i].alt,
+                                       baro + baro_offset);
+
+                       nsat = 0;
+                       if (f->gps.sats) {
+                               for (k = 0; k < f->gps.sats[j].nsat; k++) {
+                                       if (f->gps.sats[j].sat[k].svid != 0)
+                                               nsat++;
+                               }
+                               if (gps_file) {
+                                       fprintf(gps_file, " %4d", nsat);
+                                       for (k = 0; k < f->gps.sats[j].nsat; k++) {
+                                               if (f->gps.sats[j].sat[k].svid != 0) {
+                                                       fprintf (gps_file, " %3d(%4.1f)",
+                                                                f->gps.sats[j].sat[k].svid,
+                                                                (double) f->gps.sats[j].sat[k].c_n);
+                                               }
+                                       }
+                                       fprintf(gps_file, "\n");
+                               }
+                       }
+
+                       if (kml_file) {
+                               snprintf(buf, sizeof (buf), kml_coord_fmt,
+                                       f->gps.data[i].lon,
+                                       f->gps.data[i].lat,
+                                       baro + baro_offset,
+                                       f->gps.data[i].alt,
+                                       (f->gps.data[i].time - boost_start) / 100.0,
+                                       nsat);
+                               fprintf(kml_file, "%s", buf);
+                               if (state_idx + 1 < f->state.num && f->state.data[state_idx + 1].time <= f->gps.data[i].time) {
+                                       state_idx++;
+                                       if (f->state.data[state_idx - 1].value != f->state.data[state_idx].value) {
+                                               fprintf(kml_file, "%s", kml_placemark_end);
+                                               fprintf(kml_file, kml_placemark_start,
+                                                       state_names[(int)f->state.data[state_idx].value],
+                                                       state_names[(int)f->state.data[state_idx].value]); 
+                                               fprintf(kml_file, "%s", buf);
+                                       }
+                               }
+                       }
+
                }
+               if (kml_file)
+                       fprintf(kml_file, "%s", kml_footer);
        }
        if (cooked && plot_name) {
                struct cc_perioddata    *speed;
@@ -252,12 +614,20 @@ analyse_flight(struct cc_flightraw *f, FILE *summary_file, FILE *detail_file, ch
                plstar(2, 3);
                speed = merge_data(&cooked->accel_speed, &cooked->pres_speed, apogee);
 
-               plot_perioddata(&cooked->pres_pos, "meters", "Height", -1e10, 1e10);
-               plot_perioddata(&cooked->pres_pos, "meters", "Height", boost_start, apogee);
-               plot_perioddata(speed, "meters/second", "Speed", -1e10, 1e10);
-               plot_perioddata(speed, "meters/second", "Speed", boost_start, apogee);
-               plot_perioddata(&cooked->accel_accel, "meters/second²", "Acceleration", -1e10, 1e10);
-               plot_perioddata(&cooked->accel_accel, "meters/second²", "Acceleration", boost_start, apogee);
+               plot_perioddata(&cooked->pres_pos, "meters", "Height",
+                               -1e10, 1e10, PLOT_HEIGHT);
+               plot_perioddata(&cooked->pres_pos, "meters", "Height to Apogee",
+                               boost_start, apogee + (apogee - boost_start) / 10.0, PLOT_HEIGHT);
+               plot_perioddata(speed, "meters/second", "Speed",
+                               -1e10, 1e10, PLOT_SPEED);
+               plot_perioddata(speed, "meters/second", "Speed to Apogee",
+                               boost_start, apogee + (apogee - boost_start) / 10.0, PLOT_SPEED);
+               plot_perioddata(&cooked->accel_accel, "meters/second²", "Acceleration",
+                               -1e10, 1e10, PLOT_ACCEL);
+/*             plot_perioddata(&cooked->accel_accel, "meters/second²", "Acceleration during Boost",
+               boost_start, boost_stop + (boost_stop - boost_start) / 2.0, PLOT_ACCEL); */
+               plot_timedata(&cooked->accel, "meters/second²", "Acceleration during Boost",
+                               boost_start, boost_stop + (boost_stop - boost_start) / 2.0, PLOT_ACCEL);
                free(speed->data);
                free(speed);
                plend();
@@ -267,69 +637,135 @@ analyse_flight(struct cc_flightraw *f, FILE *summary_file, FILE *detail_file, ch
 }
 
 static const struct option options[] = {
-       { .name = "summary", .has_arg = 1, .val = 's' },
-       { .name = "detail", .has_arg = 1, .val = 'd' },
-       { .name = "plot", .has_arg = 1, .val = 'p' },
+       { .name = "summary", .has_arg = 2, .val = 's' },
+       { .name = "detail", .has_arg = 2, .val = 'd' },
+       { .name = "plot", .has_arg = 2, .val = 'p' },
+       { .name = "raw", .has_arg = 2, .val = 'r' },
+       { .name = "gps", .has_arg = 2, .val = 'g' },
+       { .name = "kml", .has_arg = 2, .val = 'k' },
+       { .name = "all", .has_arg = 0, .val = 'a' },
        { 0, 0, 0, 0},
 };
 
 static void usage(char *program)
 {
-       fprintf(stderr, "usage: %s [--summary=<summary-file>] [-s <summary-file>] [--detail=<detail-file] [-d <detail-file>] [--plot=<plot-file> -p <plot-file>] {flight-log} ...\n", program);
+       fprintf(stderr, "usage: %s\n"
+               "\t[--all] [-a]\n"
+               "\t[--summary=<summary-file>] [-s <summary-file>]\n"
+               "\t[--detail=<detail-file] [-d <detail-file>]\n"
+               "\t[--raw=<raw-file> -r <raw-file]\n"
+               "\t[--plot=<plot-file> -p <plot-file>]\n"
+               "\t[--gps=<gps-file> -g <gps-file>]\n"
+               "\t[--kml=<kml-file> -k <kml-file>]\n"
+               "\t{flight-log} ...\n", program);
        exit(1);
 }
 
+char *
+replace_extension(char *file, char *extension)
+{
+       char    *slash;
+       char    *dot;
+       char    *new;
+       int     newlen;
+
+       slash = strrchr(file, '/');
+       dot = strrchr(file, '.');
+       if (!dot || (slash && dot < slash))
+               dot = file + strlen(file);
+       newlen = (dot - file) + strlen (extension) + 1;
+       new = malloc (newlen);
+       strncpy (new, file, dot - file);
+       new[dot-file] = '\0';
+       strcat (new, extension);
+       return new;
+}
+
+FILE *
+open_output(char *outname, char *inname, char *extension)
+{
+       char    *o;
+       FILE    *out;
+
+       if (outname)
+               o = outname;
+       else
+               o = replace_extension(inname, extension);
+       out = fopen(o, "w");
+       if (!out) {
+               perror (o);
+               exit(1);
+       }
+       if (o != outname)
+               free(o);
+       return out;
+}
+
 int
 main (int argc, char **argv)
 {
        FILE                    *file;
-       FILE                    *summary_file;
-       FILE                    *detail_file;
+       FILE                    *summary_file = NULL;
+       FILE                    *detail_file = NULL;
+       FILE                    *raw_file = NULL;
+       FILE                    *gps_file = NULL;
+       FILE                    *kml_file = NULL;
        int                     i;
        int                     ret = 0;
        struct cc_flightraw     *raw;
        int                     c;
        int                     serial;
        char                    *s;
-       char                    *summary_name = NULL, *detail_name = NULL;
+       char                    *summary_name = NULL;
+       char                    *detail_name = NULL;
+       char                    *raw_name = NULL;
        char                    *plot_name = NULL;
+       char                    *gps_name = NULL;
+       char                    *kml_name = NULL;
+       int                     has_summary = 0;
+       int                     has_detail = 0;
+       int                     has_plot = 0;
+       int                     has_raw = 0;
+       int                     has_gps = 0;
+       int                     has_kml = 0;
+       char                    *this_plot_name = NULL;;
 
-       while ((c = getopt_long(argc, argv, "s:d:p:", options, NULL)) != -1) {
+       while ((c = getopt_long(argc, argv, "s:d:p:r:g:k:a", options, NULL)) != -1) {
                switch (c) {
                case 's':
                        summary_name = optarg;
+                       has_summary = 1;
                        break;
                case 'd':
                        detail_name = optarg;
+                       has_detail = 1;
                        break;
                case 'p':
                        plot_name = optarg;
+                       has_plot = 1;
+                       break;
+               case 'r':
+                       raw_name = optarg;
+                       has_raw = 1;
+                       break;
+               case 'g':
+                       gps_name = optarg;
+                       has_gps = 1;
+                       break;
+               case 'k':
+                       kml_name = optarg;
+                       has_kml = 1;
+                       break;
+               case 'a':
+                       has_summary = has_detail = has_plot = has_raw = has_gps = has_kml = 1;
                        break;
                default:
                        usage(argv[0]);
                        break;
                }
        }
-       summary_file = stdout;
-       detail_file = NULL;
-       if (summary_name) {
-               summary_file = fopen(summary_name, "w");
-               if (!summary_file) {
-                       perror (summary_name);
-                       exit(1);
-               }
-       }
-       if (detail_name) {
-               if (summary_name && !strcmp (summary_name, detail_name))
-                       detail_file = summary_file;
-               else {
-                       detail_file = fopen(detail_name, "w");
-                       if (!detail_file) {
-                               perror(detail_name);
-                               exit(1);
-                       }
-               }
-       }
+       if (!has_summary)
+               summary_file = stdout;
        for (i = optind; i < argc; i++) {
                file = fopen(argv[i], "r");
                if (!file) {
@@ -337,6 +773,22 @@ main (int argc, char **argv)
                        ret++;
                        continue;
                }
+               if (has_summary && !summary_file)
+                       summary_file = open_output(summary_name, argv[i], ".summary");
+               if (has_detail && !detail_file)
+                       detail_file = open_output(detail_name, argv[i], ".detail");
+               if (has_plot) {
+                       if (plot_name)
+                               this_plot_name = plot_name;
+                       else
+                               this_plot_name = replace_extension(argv[i], ".plot");
+               }
+               if (has_raw && !raw_file)
+                       raw_file = open_output(raw_name, argv[i], ".raw");
+               if (has_gps && !gps_file)
+                       gps_file = open_output(gps_name, argv[i], ".gps");
+               if (has_kml && !kml_file)
+                       kml_file = open_output(kml_name, argv[i], ".kml");
                s = strstr(argv[i], "-serial-");
                if (s)
                        serial = atoi(s + 8);
@@ -350,8 +802,26 @@ main (int argc, char **argv)
                }
                if (!raw->serial)
                        raw->serial = serial;
-               analyse_flight(raw, summary_file, detail_file, plot_name);
+               analyse_flight(raw, summary_file, detail_file, raw_file, this_plot_name, gps_file, kml_file);
                cc_flightraw_free(raw);
+               if (has_summary && !summary_name) {
+                       fclose(summary_file); summary_file = NULL;
+               }
+               if (has_detail && !detail_name) {
+                       fclose(detail_file); detail_file = NULL;
+               }
+               if (this_plot_name && this_plot_name != plot_name) {
+                       free (this_plot_name); this_plot_name = NULL;
+               }
+               if (has_raw && !raw_name) {
+                       fclose(raw_file); raw_file = NULL;
+               }
+               if (has_gps && !gps_name) {
+                       fclose(gps_file); gps_file = NULL;
+               }
+               if (has_kml && !kml_name) {
+                       fclose(kml_file); kml_file = NULL;
+               }
        }
        return ret;
 }