Altosui: Add flight statistics tab to graph window
[fw/altos] / altosui / AltosState.java
1 /*
2  * Copyright © 2010 Keith Packard <keithp@keithp.com>
3  *
4  * This program is free software; you can redistribute it and/or modify
5  * it under the terms of the GNU General Public License as published by
6  * the Free Software Foundation; version 2 of the License.
7  *
8  * This program is distributed in the hope that it will be useful, but
9  * WITHOUT ANY WARRANTY; without even the implied warranty of
10  * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the GNU
11  * General Public License for more details.
12  *
13  * You should have received a copy of the GNU General Public License along
14  * with this program; if not, write to the Free Software Foundation, Inc.,
15  * 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA.
16  */
17
18 /*
19  * Track flight state from telemetry or eeprom data stream
20  */
21
22 package altosui;
23
24 public class AltosState {
25         AltosRecord data;
26
27         /* derived data */
28
29         long    report_time;
30
31         double  time;
32         double  time_change;
33         int     tick;
34
35         int     state;
36         boolean landed;
37         boolean ascent; /* going up? */
38
39         double  ground_altitude;
40         double  height;
41         double  speed;
42         double  acceleration;
43         double  battery;
44         double  temperature;
45         double  main_sense;
46         double  drogue_sense;
47         double  baro_speed;
48
49         double  max_height;
50         double  max_acceleration;
51         double  max_speed;
52
53         AltosGPS        gps;
54
55         double  pad_lat;
56         double  pad_lon;
57         double  pad_alt;
58
59         static final int MIN_PAD_SAMPLES = 10;
60
61         int     npad;
62         int     ngps;
63         int     gps_waiting;
64         boolean gps_ready;
65
66         AltosGreatCircle from_pad;
67         double  elevation;      /* from pad */
68         double  range;          /* total distance */
69
70         double  gps_height;
71
72         int     speak_tick;
73         double  speak_altitude;
74
75
76         void init (AltosRecord cur, AltosState prev_state) {
77                 int             i;
78                 AltosRecord prev;
79
80                 data = cur;
81
82                 ground_altitude = data.ground_altitude();
83                 height = data.filtered_height();
84
85                 report_time = System.currentTimeMillis();
86
87                 acceleration = data.acceleration();
88                 speed = data.accel_speed();
89                 temperature = data.temperature();
90                 drogue_sense = data.drogue_voltage();
91                 main_sense = data.main_voltage();
92                 battery = data.battery_voltage();
93                 tick = data.tick;
94                 state = data.state;
95
96                 if (prev_state != null) {
97
98                         /* Preserve any existing gps data */
99                         npad = prev_state.npad;
100                         ngps = prev_state.ngps;
101                         gps = prev_state.gps;
102                         pad_lat = prev_state.pad_lat;
103                         pad_lon = prev_state.pad_lon;
104                         pad_alt = prev_state.pad_alt;
105                         max_height = prev_state.max_height;
106                         max_acceleration = prev_state.max_acceleration;
107                         max_speed = prev_state.max_speed;
108
109                         /* make sure the clock is monotonic */
110                         while (tick < prev_state.tick)
111                                 tick += 65536;
112
113                         time_change = (tick - prev_state.tick) / 100.0;
114
115                         /* compute barometric speed */
116
117                         double height_change = height - prev_state.height;
118                         if (data.speed != AltosRecord.MISSING)
119                                 baro_speed = data.speed;
120                         else {
121                                 if (time_change > 0)
122                                         baro_speed = (prev_state.baro_speed * 3 + (height_change / time_change)) / 4.0;
123                                 else
124                                         baro_speed = prev_state.baro_speed;
125                         }
126                 } else {
127                         npad = 0;
128                         ngps = 0;
129                         gps = null;
130                         baro_speed = 0;
131                         time_change = 0;
132                 }
133
134                 time = tick / 100.0;
135
136                 if (state == Altos.ao_flight_pad || state == Altos.ao_flight_idle) {
137
138                         /* Track consecutive 'good' gps reports, waiting for 10 of them */
139                         if (data.gps != null && data.gps.locked && data.gps.nsat >= 4)
140                                 npad++;
141                         else
142                                 npad = 0;
143
144                         /* Average GPS data while on the pad */
145                         if (data.gps != null && data.gps.locked && data.gps.nsat >= 4) {
146                                 if (ngps > 1) {
147                                         /* filter pad position */
148                                         pad_lat = (pad_lat * 31.0 + data.gps.lat) / 32.0;
149                                         pad_lon = (pad_lon * 31.0 + data.gps.lon) / 32.0;
150                                         pad_alt = (pad_alt * 31.0 + data.gps.alt) / 32.0;
151                                 } else {
152                                         pad_lat = data.gps.lat;
153                                         pad_lon = data.gps.lon;
154                                         pad_alt = data.gps.alt;
155                                 }
156                                 ngps++;
157                         }
158                 }
159
160                 gps_waiting = MIN_PAD_SAMPLES - npad;
161                 if (gps_waiting < 0)
162                         gps_waiting = 0;
163
164                 gps_ready = gps_waiting == 0;
165
166                 ascent = (Altos.ao_flight_boost <= state &&
167                           state <= Altos.ao_flight_coast);
168
169                 /* Only look at accelerometer data on the way up */
170                 if (ascent && acceleration > max_acceleration)
171                         max_acceleration = acceleration;
172                 if (ascent && speed > max_speed)
173                         max_speed = speed;
174
175                 if (height > max_height)
176                         max_height = height;
177                 if (data.gps != null) {
178                         if (gps == null || !gps.locked || data.gps.locked)
179                                 gps = data.gps;
180                         if (ngps > 0 && gps.locked) {
181                                 from_pad = new AltosGreatCircle(pad_lat, pad_lon, gps.lat, gps.lon);
182                         }
183                 }
184                 elevation = 0;
185                 range = -1;
186                 if (ngps > 0) {
187                         gps_height = gps.alt - pad_alt;
188                         if (from_pad != null) {
189                                 elevation = Math.atan2(height, from_pad.distance) * 180 / Math.PI;
190                                 range = Math.sqrt(height * height + from_pad.distance * from_pad.distance);
191                         }
192                 } else {
193                         gps_height = 0;
194                 }
195         }
196
197         public AltosState(AltosRecord cur) {
198                 init(cur, null);
199         }
200
201         public AltosState (AltosRecord cur, AltosState prev) {
202                 init(cur, prev);
203         }
204 }