+ public void info_add_deg(int col, String name, double v, int pos, int neg) {
+ int c = pos;
+ if (v < 0) {
+ c = neg;
+ v = -v;
+ }
+ double deg = Math.floor(v);
+ double min = (v - deg) * 60;
+
+ flightInfoModel[col].addRow(name, String.format("%3.0f°%08.5f'", deg, min));
+ }
+
+ public void info_finish() {
+ for (int i = 0; i < info_columns; i++)
+ flightInfoModel[i].finish();
+ }
+
+ public void show(AltosState state) {
+ flightStatusModel.set(state);
+
+ info_reset();
+ if (state.gps_ready)
+ info_add_row(0, "Ground state", "%s", "ready");
+ else
+ info_add_row(0, "Ground state", "wait (%d)",
+ state.gps_waiting);
+ info_add_row(0, "Rocket state", "%s", state.data.state);
+ info_add_row(0, "Callsign", "%s", state.data.callsign);
+ info_add_row(0, "Rocket serial", "%6d", state.data.serial);
+ info_add_row(0, "Rocket flight", "%6d", state.data.flight);
+
+ info_add_row(0, "RSSI", "%6d dBm", state.data.rssi);
+ info_add_row(0, "Height", "%6.0f m", state.height);
+ info_add_row(0, "Max height", "%6.0f m", state.max_height);
+ info_add_row(0, "Acceleration", "%8.1f m/s²", state.acceleration);
+ info_add_row(0, "Max acceleration", "%8.1f m/s²", state.max_acceleration);
+ info_add_row(0, "Speed", "%8.1f m/s", state.ascent ? state.speed : state.baro_speed);
+ info_add_row(0, "Max Speed", "%8.1f m/s", state.max_speed);
+ info_add_row(0, "Temperature", "%9.2f °C", state.temperature);
+ info_add_row(0, "Battery", "%9.2f V", state.battery);
+ info_add_row(0, "Drogue", "%9.2f V", state.drogue_sense);
+ info_add_row(0, "Main", "%9.2f V", state.main_sense);
+ info_add_row(0, "Pad altitude", "%6.0f m", state.ground_altitude);
+ if (state.gps == null) {
+ info_add_row(1, "GPS", "not available");
+ } else {
+ if (state.data.gps.gps_locked)
+ info_add_row(1, "GPS", " locked");
+ else if (state.data.gps.gps_connected)
+ info_add_row(1, "GPS", " unlocked");
+ else
+ info_add_row(1, "GPS", " missing");
+ info_add_row(1, "Satellites", "%6d", state.data.gps.nsat);
+ info_add_deg(1, "Latitude", state.gps.lat, 'N', 'S');
+ info_add_deg(1, "Longitude", state.gps.lon, 'E', 'W');
+ info_add_row(1, "GPS altitude", "%6d", state.gps.alt);
+ info_add_row(1, "GPS height", "%6.0f", state.gps_height);
+
+ /* The SkyTraq GPS doesn't report these values */
+ if (false) {
+ info_add_row(1, "GPS ground speed", "%8.1f m/s %3d°",
+ state.gps.ground_speed,
+ state.gps.course);
+ info_add_row(1, "GPS climb rate", "%8.1f m/s",
+ state.gps.climb_rate);
+ info_add_row(1, "GPS error", "%6d m(h)%3d m(v)",
+ state.gps.h_error, state.gps.v_error);
+ }
+ info_add_row(1, "GPS hdop", "%8.1f", state.gps.hdop);
+
+ if (state.npad > 0) {
+ if (state.from_pad != null) {
+ info_add_row(1, "Distance from pad", "%6.0f m", state.from_pad.distance);
+ info_add_row(1, "Direction from pad", "%6.0f°", state.from_pad.bearing);
+ } else {
+ info_add_row(1, "Distance from pad", "unknown");
+ info_add_row(1, "Direction from pad", "unknown");
+ }
+ info_add_deg(1, "Pad latitude", state.pad_lat, 'N', 'S');
+ info_add_deg(1, "Pad longitude", state.pad_lon, 'E', 'W');
+ info_add_row(1, "Pad GPS alt", "%6.0f m", state.pad_alt);
+ }
+ info_add_row(1, "GPS date", "%04d-%02d-%02d",
+ state.gps.year,
+ state.gps.month,
+ state.gps.day);
+ info_add_row(1, "GPS time", " %02d:%02d:%02d",
+ state.gps.hour,
+ state.gps.minute,
+ state.gps.second);
+ int nsat_vis = 0;
+ int c;
+
+ if (state.gps.cc_gps_sat == null)
+ info_add_row(2, "Satellites Visible", "%4d", 0);
+ else {
+ info_add_row(2, "Satellites Visible", "%4d", state.gps.cc_gps_sat.length);
+ for (c = 0; c < state.gps.cc_gps_sat.length; c++) {
+ info_add_row(2, "Satellite id,C/N0",
+ "%4d, %4d",
+ state.gps.cc_gps_sat[c].svid,
+ state.gps.cc_gps_sat[c].c_n0);
+ }
+ }
+ }
+ info_finish();
+ }
+
+ class IdleThread extends Thread {
+
+ private AltosState state;
+ int reported_landing;
+
+ public void report(boolean last) {
+ if (state == null)
+ return;