*
* 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.
+ * the Free Software Foundation; either version 2 of the License, or
+ * (at your option) any later version.
*
* This program is distributed in the hope that it will be useful, but
* WITHOUT ANY WARRANTY; without even the implied warranty of
*/
for (i = 0; i < raw->state.num; i++) {
if (!start_set && raw->state.data[i].value > ao_flight_pad) {
- flight_start = raw->state.data[i].time;
+ flight_start = raw->state.data[i].time - 10;
start_set = 1;
}
if (!stop_set && raw->state.data[i].value > ao_flight_main) {
}
}
- if (!start_set)
+ if (!start_set || flight_start < raw->accel.data[0].time)
flight_start = raw->accel.data[0].time;
if (stop_set) {
for (i = 0; i < raw->accel.num - 1; i++) {
accel_speed = cc_timedata_integrate(&cooked->accel, flight_start - 10, flight_stop);
accel_pos = cc_timedata_integrate(accel_speed, flight_start - 10, flight_stop);
-#define ACCEL_OMEGA_PASS (2 * M_PI * 5 / 100)
-#define ACCEL_OMEGA_STOP (2 * M_PI * 8 / 100)
+#define ACCEL_OMEGA_PASS (2 * M_PI * 20 / 100)
+#define ACCEL_OMEGA_STOP (2 * M_PI * 30 / 100)
#define BARO_OMEGA_PASS (2 * M_PI * .5 / 100)
#define BARO_OMEGA_STOP (2 * M_PI * 1 / 100)
#define FILTER_ERROR (1e-8)