diff options
| author | Keith Packard <keithp@keithp.com> | 2012-04-14 12:02:14 -0700 |
|---|---|---|
| committer | Keith Packard <keithp@keithp.com> | 2012-04-14 14:04:29 -0700 |
| commit | 6cb744e305116a738b5d71686c6748f6f08c12ea (patch) | |
| tree | 536b510332adb5dd93f99c8c06b33a18b038d832 /src/test/ao_flight_test.c | |
| parent | 9a8fec1b6d8f3346f988882ffb03d7d0e45b3c81 (diff) | |
altos: Respect apogee lockout time in flight algorithm
This prevents any apogee detection from occurring until the specified
number of seconds after boost. This also prevents the switch from
accel+baro to baro only mode in the Kalman filter.
The test frame work is also changed to look for Apogee lockout: in the
eeprom input file.
Signed-off-by: Keith Packard <keithp@keithp.com>
Diffstat (limited to 'src/test/ao_flight_test.c')
| -rw-r--r-- | src/test/ao_flight_test.c | 4 |
1 files changed, 4 insertions, 0 deletions
diff --git a/src/test/ao_flight_test.c b/src/test/ao_flight_test.c index 921d44e7..4a8625cf 100644 --- a/src/test/ao_flight_test.c +++ b/src/test/ao_flight_test.c @@ -184,6 +184,7 @@ struct ao_config { int16_t accel_plus_g; int16_t accel_minus_g; uint8_t pad_orientation; + uint16_t apogee_lockout; }; #define AO_PAD_ORIENTATION_ANTENNA_UP 0 @@ -523,6 +524,9 @@ ao_sleep(void *wchan) ao_config.accel_minus_g = atoi(words[5]); } else if (nword >= 4 && strcmp(words[0], "Main") == 0) { ao_config.main_deploy = atoi(words[2]); + } else if (nword >= 3 && strcmp(words[0], "Apogee") == 0 && + strcmp(words[1], "lockout:") == 0) { + ao_config.apogee_lockout = atoi(words[2]); } else if (nword >= 36 && strcmp(words[0], "CALL") == 0) { tick = atoi(words[10]); if (!ao_flight_started) { |