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/*
* Copyright © 2010 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.
*/
package altosui;
import java.awt.*;
import java.awt.event.*;
import javax.swing.*;
import javax.swing.filechooser.FileNameExtensionFilter;
import javax.swing.table.*;
import java.io.*;
import java.util.*;
import java.text.*;
import java.util.prefs.*;
import java.util.concurrent.LinkedBlockingQueue;
import altosui.AltosFlightInfoTableModel;
import altosui.AltosState;
public class AltosInfoTable {
private Box box;
private JTable table[];
private AltosFlightInfoTableModel model[];
private Box ibox[];
private Font infoLabelFont = new Font("SansSerif", Font.PLAIN, 14);
private Font infoValueFont = new Font("Monospaced", Font.PLAIN, 14);
static final int info_columns = 3;
static final int info_rows = 17;
public AltosInfoTable() {
box = Box.createHorizontalBox();
model = new AltosFlightInfoTableModel[info_columns];
table = new JTable[info_columns];
ibox = new Box[info_columns];
for (int i = 0; i < info_columns; i++) {
model[i] = new AltosFlightInfoTableModel();
table[i] = new JTable(model[i]);
ibox[i] = box.createVerticalBox();
table[i].setFont(infoValueFont);
table[i].setRowHeight(rowHeight());
table[i].setShowGrid(true);
ibox[i].add(table[i].getTableHeader());
ibox[i].add(table[i]);
box.add(ibox[i]);
}
}
public int rowHeight() {
FontMetrics infoValueMetrics = table[0].getFontMetrics(infoValueFont);
return (infoValueMetrics.getHeight() + infoValueMetrics.getLeading()) * 20 / 10;
}
public int columnWidth() {
FontMetrics infoValueMetrics = table[0].getFontMetrics(infoValueFont);
return infoValueMetrics.charWidth('0') * 20 * 2;
}
public int height() {
return rowHeight() * info_rows;
}
public int width() {
return columnWidth() * info_columns;
}
public Box box() {
return box;
}
void info_reset() {
for (int i = 0; i < info_columns; i++)
model[i].resetRow();
}
void info_add_row(int col, String name, String value) {
model[col].addRow(name, value);
}
void info_add_row(int col, String name, String format, Object... parameters) {
model[col].addRow(name, String.format(format, parameters));
}
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;
model[col].addRow(name, String.format("%3.0f°%08.5f'", deg, min));
}
void info_finish() {
for (int i = 0; i < info_columns; i++)
model[i].finish();
}
public void clear() {
info_reset();
info_finish();
}
public void show(AltosState state, int crc_errors) {
if (state == null)
return;
info_reset();
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, "CRC Errors", "%6d", crc_errors);
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.gps_ready)
info_add_row(1, "GPS state", "%s", "ready");
else
info_add_row(1, "GPS state", "wait (%d)",
state.gps_waiting);
if (state.data.gps.locked)
info_add_row(1, "GPS", " locked");
else if (state.data.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", "%6d m",
(int) (state.from_pad.distance + 0.5));
info_add_row(1, "Direction from pad", "%6d°",
(int) (state.from_pad.bearing + 0.5));
info_add_row(1, "Elevation from pad", "%6d°",
(int) (state.elevation + 0.5));
info_add_row(1, "Range from pad", "%6d m",
(int) (state.range + 0.5));
} else {
info_add_row(1, "Distance from pad", "unknown");
info_add_row(1, "Direction from pad", "unknown");
info_add_row(1, "Elevation from pad", "unknown");
info_add_row(1, "Range 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();
}
}
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