Initial Commit - Copy from Altus Metrum AltOS
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299
altosuilib/AltosInfoTable.java
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299
altosuilib/AltosInfoTable.java
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/*
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* Copyright © 2010 Keith Packard <keithp@keithp.com>
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*
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* This program is free software; you can redistribute it and/or modify
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* it under the terms of the GNU General Public License as published by
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* the Free Software Foundation; either version 2 of the License, or
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* (at your option) any later version.
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*
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* This program is distributed in the hope that it will be useful, but
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* WITHOUT ANY WARRANTY; without even the implied warranty of
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* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
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* General Public License for more details.
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*
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* You should have received a copy of the GNU General Public License along
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* with this program; if not, write to the Free Software Foundation, Inc.,
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* 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA.
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*/
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package org.altusmetrum.altosuilib_14;
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import java.awt.*;
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import java.awt.event.*;
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import javax.swing.*;
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import javax.swing.table.*;
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import org.altusmetrum.altoslib_14.*;
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public class AltosInfoTable extends JTable implements AltosFlightDisplay, HierarchyListener {
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private AltosFlightInfoTableModel model;
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static final int info_columns = 4;
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static final int info_rows = 18;
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private AltosState last_state;
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private AltosListenerState last_listener_state;
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int desired_row_height() {
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FontMetrics infoValueMetrics = getFontMetrics(AltosUILib.table_value_font);
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return (infoValueMetrics.getHeight() + infoValueMetrics.getLeading()) * 18 / 10;
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}
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int text_width(String t) {
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FontMetrics infoValueMetrics = getFontMetrics(AltosUILib.table_value_font);
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return infoValueMetrics.stringWidth(t);
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}
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void set_layout() {
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setRowHeight(desired_row_height());
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for (int i = 0; i < info_columns * 2; i++)
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{
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TableColumn column = getColumnModel().getColumn(i);
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if ((i & 1) == 0)
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column.setPreferredWidth(text_width(" Satellites Visible"));
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else
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column.setPreferredWidth(text_width("W 179°59.99999' "));
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}
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}
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public AltosInfoTable() {
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super(new AltosFlightInfoTableModel(info_rows, info_columns));
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model = (AltosFlightInfoTableModel) getModel();
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setFont(AltosUILib.table_value_font);
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addHierarchyListener(this);
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setAutoResizeMode(AUTO_RESIZE_ALL_COLUMNS);
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setShowGrid(true);
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set_layout();
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doLayout();
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}
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public void font_size_changed(int font_size) {
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setFont(AltosUILib.table_value_font);
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set_layout();
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doLayout();
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}
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public void units_changed(boolean imperial_units) {
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}
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public void hierarchyChanged(HierarchyEvent e) {
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if (last_state != null && isShowing()) {
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AltosState state = last_state;
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AltosListenerState listener_state = last_listener_state;
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last_state = null;
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last_listener_state = null;
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show(state, listener_state);
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}
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}
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public Dimension getPreferredScrollableViewportSize() {
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return getPreferredSize();
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}
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public void reset() {
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model.reset();
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}
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void info_add_row(int col, String name, String value) {
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model.addRow(col, name, value);
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}
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void info_add_row(int col, String name, String format, Object... parameters) {
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info_add_row (col, name, String.format(format, parameters));
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}
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void info_add_deg(int col, String name, double v, int pos, int neg) {
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int c = pos;
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if (v < 0) {
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c = neg;
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v = -v;
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}
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double deg = Math.floor(v);
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double min = (v - deg) * 60;
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info_add_row(col, name, String.format("%c %3.0f°%08.5f'", c, deg, min));
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}
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void info_finish() {
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model.finish();
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}
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public void clear() {
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model.clear();
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}
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public String getName() { return "Table"; }
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public void show(AltosState state, AltosListenerState listener_state) {
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AltosCalData cal_data = state.cal_data();
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if (!isShowing()) {
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last_state = state;
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last_listener_state = listener_state;
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return;
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}
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reset();
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if (state != null) {
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if (cal_data.device_type != AltosLib.MISSING)
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info_add_row(0, "Device", "%s", AltosLib.product_name(cal_data.device_type));
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else if (cal_data.product != null)
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info_add_row(0, "Device", "%s", cal_data.product);
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if (state.tick() != AltosLib.MISSING)
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info_add_row(0, "Tick", "%6d", state.tick());
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if (state.altitude() != AltosLib.MISSING)
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info_add_row(0, "Altitude", "%6.0f m", state.altitude());
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if (cal_data.ground_altitude != AltosLib.MISSING)
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info_add_row(0, "Pad altitude", "%6.0f m", cal_data.ground_altitude);
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if (state.height() != AltosLib.MISSING)
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info_add_row(0, "Height", "%6.0f m", state.height());
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if (state.max_height() != AltosLib.MISSING)
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info_add_row(0, "Max height", "%6.0f m", state.max_height());
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if (state.acceleration() != AltosLib.MISSING)
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info_add_row(0, "Acceleration", "%8.1f m/s²", state.acceleration());
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if (state.max_acceleration() != AltosLib.MISSING)
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info_add_row(0, "Max acceleration", "%8.1f m/s²", state.max_acceleration());
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if (state.speed() != AltosLib.MISSING)
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info_add_row(0, "Speed", "%8.1f m/s", state.speed());
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if (state.max_speed() != AltosLib.MISSING)
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info_add_row(0, "Max Speed", "%8.1f m/s", state.max_speed());
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if (state.orient() != AltosLib.MISSING)
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info_add_row(0, "Tilt", "%4.0f °", state.orient());
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if (state.max_orient() != AltosLib.MISSING)
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info_add_row(0, "Max Tilt", "%4.0f °", state.max_orient());
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if (state.temperature != AltosLib.MISSING)
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info_add_row(0, "Temperature", "%9.2f °C", state.temperature);
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if (state.battery_voltage != AltosLib.MISSING)
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info_add_row(0, "Battery", "%9.2f V", state.battery_voltage);
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if (state.apogee_voltage != AltosLib.MISSING)
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info_add_row(0, "Drogue", "%9.2f V", state.apogee_voltage);
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if (state.main_voltage != AltosLib.MISSING)
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info_add_row(0, "Main", "%9.2f V", state.main_voltage);
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}
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if (listener_state != null) {
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info_add_row(0, "CRC Errors", "%6d", listener_state.crc_errors);
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if (listener_state.battery != AltosLib.MISSING)
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info_add_row(0, "Receiver Battery", "%9.2f", listener_state.battery);
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}
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if (state != null) {
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if (state.gps == null || !state.gps.connected) {
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info_add_row(1, "GPS", "not available");
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} else {
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if (state.gps_ready)
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info_add_row(1, "GPS state", "%s", "ready");
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else
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info_add_row(1, "GPS state", "wait (%d)",
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state.gps_waiting);
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if (state.gps.locked)
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info_add_row(1, "GPS", " locked");
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else if (state.gps.connected)
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info_add_row(1, "GPS", " unlocked");
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else
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info_add_row(1, "GPS", " missing");
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info_add_row(1, "Satellites", "%6d", state.gps.nsat);
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if (state.gps.lat != AltosLib.MISSING)
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info_add_deg(1, "Latitude", state.gps.lat, 'N', 'S');
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if (state.gps.lon != AltosLib.MISSING)
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info_add_deg(1, "Longitude", state.gps.lon, 'E', 'W');
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if (state.gps.alt != AltosLib.MISSING)
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info_add_row(1, "GPS altitude", "%8.1f m", state.gps.alt);
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if (state.gps_height != AltosLib.MISSING)
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info_add_row(1, "GPS height", "%8.1f m", state.gps_height);
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if (state.gps.ground_speed != AltosLib.MISSING && state.gps.course != AltosLib.MISSING)
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info_add_row(1, "GPS ground speed", "%6.1f m/s %3d°",
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state.gps.ground_speed,
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state.gps.course);
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if (state.gps.climb_rate != AltosLib.MISSING)
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info_add_row(1, "GPS climb rate", "%6.1f m/s",
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state.gps.climb_rate);
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if (state.gps.h_error != AltosLib.MISSING && state.gps.v_error != AltosLib.MISSING)
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info_add_row(1, "GPS error", "%6.0f m(h)%6.0f m(v)",
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state.gps.h_error, state.gps.v_error);
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if (state.gps.pdop != AltosLib.MISSING &&
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state.gps.hdop != AltosLib.MISSING &&
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state.gps.vdop != AltosLib.MISSING)
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info_add_row(1, "GPS dop", "%3.1fp/%3.1fh/%3.1fv",
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state.gps.pdop,
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state.gps.hdop,
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state.gps.vdop);
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if (state.npad > 0) {
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if (state.from_pad != null) {
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info_add_row(1, "Ground pad dist", "%6d m",
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(int) (state.from_pad.distance + 0.5));
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info_add_row(1, "Direction from pad", "%6d°",
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(int) (state.from_pad.bearing + 0.5));
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info_add_row(1, "Elevation from pad", "%6d°",
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(int) (state.elevation + 0.5));
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info_add_row(1, "Range from pad", "%6d m",
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(int) (state.range + 0.5));
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} else {
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info_add_row(1, "Distance from pad", "unknown");
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info_add_row(1, "Direction from pad", "unknown");
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info_add_row(1, "Elevation from pad", "unknown");
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info_add_row(1, "Range from pad", "unknown");
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}
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info_add_deg(1, "Pad latitude", state.pad_lat, 'N', 'S');
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info_add_deg(1, "Pad longitude", state.pad_lon, 'E', 'W');
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info_add_row(1, "Pad GPS alt", "%6.0f m", state.gps_ground_altitude());
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}
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if (state.gps.year != AltosLib.MISSING)
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info_add_row(2, "GPS date", "%04d-%02d-%02d",
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state.gps.year,
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state.gps.month,
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state.gps.day);
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if (state.gps.hour != AltosLib.MISSING)
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info_add_row(2, "GPS time", " %02d:%02d:%02d",
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state.gps.hour,
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state.gps.minute,
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state.gps.second);
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//int nsat_vis = 0;
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int c;
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if (state.gps.cc_gps_sat == null)
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info_add_row(2, "Satellites Visible", "%4d", 0);
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else {
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info_add_row(2, "Satellites Visible", "%4d", state.gps.cc_gps_sat.length);
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for (c = 0; c < state.gps.cc_gps_sat.length; c++) {
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info_add_row(2, "Satellite id,C/N0",
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"%4d, %4d",
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state.gps.cc_gps_sat[c].svid,
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state.gps.cc_gps_sat[c].c_n0);
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}
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}
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}
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}
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if (state != null && state.accel_along() != AltosLib.MISSING) {
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info_add_row(3, "Accel along", "%8.1f m/s²", state.accel_along());
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info_add_row(3, "Accel across", "%8.1f m/s²", state.accel_across());
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info_add_row(3, "Accel through", "%8.1f m/s²", state.accel_through());
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}
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if (state != null && state.gyro_roll() != AltosLib.MISSING) {
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info_add_row(3, "Gyro roll", "%8.1f °/s", state.gyro_roll());
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info_add_row(3, "Gyro pitch", "%8.1f °/s", state.gyro_pitch());
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info_add_row(3, "Gyro yaw", "%8.1f °/s", state.gyro_yaw());
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}
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if (state != null && state.mag_along() != AltosLib.MISSING) {
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/* Report mag in nanoteslas (1 G = 100000 nT (or γ)) */
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info_add_row(3, "Mag along", "%8.1f µT", state.mag_along() * 100.0);
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info_add_row(3, "Mag across", "%8.1f µT", state.mag_across() * 100.0);
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info_add_row(3, "Mag Through", "%8.1f µT", state.mag_through() * 100.0);
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info_add_row(3, "Mag Bearing", "%8.1f°", Math.atan2(state.mag_across(), state.mag_through()) * 180/Math.PI);
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}
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if (state != null && state.igniter_voltage != null) {
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for (int i = 0; i < state.igniter_voltage.length; i++)
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info_add_row(3, AltosLib.igniter_name(i), "%9.2f V", state.igniter_voltage[i]);
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}
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info_finish();
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}
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}
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