X-Git-Url: https://git.gag.com/?p=fw%2Faltos;a=blobdiff_plain;f=altosui%2FAltosFlightStats.java;h=967f094f3516322f3660416d0d09b9f636324ca5;hp=ab094c805d6e0d53ee7ef7ff2fe97854b87ba3f2;hb=5a3c5de6657d1c26e52015a8acec0cd05e294cef;hpb=95268d681c9a6652d84db383f55a4fe8a4ac5173 diff --git a/altosui/AltosFlightStats.java b/altosui/AltosFlightStats.java index ab094c80..967f094f 100644 --- a/altosui/AltosFlightStats.java +++ b/altosui/AltosFlightStats.java @@ -17,23 +17,14 @@ 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.*; -import org.altusmetrum.AltosLib.*; +import org.altusmetrum.altoslib.*; public class AltosFlightStats { double max_height; double max_speed; double max_acceleration; - double[] state_speed = new double[Altos.ao_flight_invalid + 1]; + double[] state_accel_speed = new double[Altos.ao_flight_invalid + 1]; double[] state_baro_speed = new double[Altos.ao_flight_invalid + 1]; double[] state_accel = new double[Altos.ao_flight_invalid + 1]; int[] state_count = new int[Altos.ao_flight_invalid + 1]; @@ -132,7 +123,7 @@ public class AltosFlightStats { } } state_accel[state.state] += state.acceleration; - state_speed[state.state] += state.speed; + state_accel_speed[state.state] += state.accel_speed; state_baro_speed[state.state] += state.baro_speed; state_count[state.state]++; if (state_start[state.state] == 0.0) @@ -140,8 +131,8 @@ public class AltosFlightStats { if (state_end[state.state] < state.time) state_end[state.state] = state.time; max_height = state.max_height; - if (state.max_speed != 0) - max_speed = state.max_speed; + if (state.max_accel_speed != 0) + max_speed = state.max_accel_speed; else max_speed = state.max_baro_speed; max_acceleration = state.max_acceleration; @@ -149,7 +140,7 @@ public class AltosFlightStats { } for (int s = Altos.ao_flight_startup; s <= Altos.ao_flight_landed; s++) { if (state_count[s] > 0) { - state_speed[s] /= state_count[s]; + state_accel_speed[s] /= state_count[s]; state_baro_speed[s] /= state_count[s]; state_accel[s] /= state_count[s]; }