X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=src%2Fkernel%2Fao_kalman.c;h=f93f5aba94f1daa17d2830d7ce42969e6617111e;hb=07eecc0ff6e1104f911e5f83d67f3e14dc68c59c;hp=e4cc6d4b9f73676fbc93b750ececfad91b2ed332;hpb=e56e1dc20b3bf18073766da4e26e97d9e1d419fc;p=fw%2Faltos diff --git a/src/kernel/ao_kalman.c b/src/kernel/ao_kalman.c index e4cc6d4b..f93f5aba 100644 --- a/src/kernel/ao_kalman.c +++ b/src/kernel/ao_kalman.c @@ -24,9 +24,9 @@ #include "ao_sample.h" #include "ao_kalman.h" -static __pdata ao_k_t ao_k_height; -static __pdata ao_k_t ao_k_speed; -static __pdata ao_k_t ao_k_accel; +static ao_k_t ao_k_height; +static ao_k_t ao_k_speed; +static ao_k_t ao_k_accel; #define AO_K_STEP_100 to_fix_v(0.01) #define AO_K_STEP_2_2_100 to_fix_v(0.00005) @@ -37,24 +37,24 @@ static __pdata ao_k_t ao_k_accel; #define AO_K_STEP_1 to_fix_v(1) #define AO_K_STEP_2_2_1 to_fix_v(0.5) -__pdata ao_v_t ao_height; -__pdata ao_v_t ao_speed; -__pdata ao_v_t ao_accel; -__xdata ao_v_t ao_max_height; -static __pdata ao_k_t ao_avg_height_scaled; -__xdata ao_v_t ao_avg_height; +ao_v_t ao_height; +ao_v_t ao_speed; +ao_v_t ao_accel; +ao_v_t ao_max_height; +static ao_k_t ao_avg_height_scaled; +ao_v_t ao_avg_height; -__pdata ao_v_t ao_error_h; +ao_v_t ao_error_h; #if !HAS_ACCEL || AO_FLIGHT_TEST #define AO_ERROR_H_SQ_AVG 1 #endif #if AO_ERROR_H_SQ_AVG -__pdata ao_v_t ao_error_h_sq_avg; +ao_v_t ao_error_h_sq_avg; #endif #if HAS_ACCEL -__pdata ao_v_t ao_error_a; +ao_v_t ao_error_a; #endif static void @@ -86,6 +86,7 @@ ao_kalman_predict(void) ao_k_speed += (ao_k_t) ao_accel * AO_K_STEP_100; } +#if HAS_BARO static void ao_kalman_err_height(void) { @@ -140,7 +141,9 @@ ao_kalman_err_height(void) #endif } } +#endif +#if HAS_BARO static void ao_kalman_correct_baro(void) { @@ -163,6 +166,7 @@ ao_kalman_correct_baro(void) ao_k_speed += (ao_k_t) AO_BARO_K1_100 * ao_error_h; ao_k_accel += (ao_k_t) AO_BARO_K2_100 * ao_error_h; } +#endif #if HAS_ACCEL @@ -177,7 +181,7 @@ ao_kalman_err_accel(void) ao_error_a = (accel - ao_k_accel) >> 16; } -#ifndef FORCE_ACCEL +#if !defined(FORCE_ACCEL) && HAS_BARO static void ao_kalman_correct_both(void) { @@ -255,12 +259,14 @@ ao_kalman_correct_accel(void) { ao_kalman_err_accel(); +#ifdef AO_FLIGHT_TEST if ((int16_t) (ao_sample_tick - ao_sample_prev_tick) > 5) { ao_k_height +=(ao_k_t) AO_ACCEL_K0_10 * ao_error_a; ao_k_speed += (ao_k_t) AO_ACCEL_K1_10 * ao_error_a; ao_k_accel += (ao_k_t) AO_ACCEL_K2_10 * ao_error_a; return; } +#endif ao_k_height += (ao_k_t) AO_ACCEL_K0_100 * ao_error_a; ao_k_speed += (ao_k_t) AO_ACCEL_K1_100 * ao_error_a; ao_k_accel += (ao_k_t) AO_ACCEL_K2_100 * ao_error_a; @@ -269,10 +275,30 @@ ao_kalman_correct_accel(void) #endif /* else FORCE_ACCEL */ #endif /* HAS_ACCEL */ +#if !HAS_BARO +static ao_k_t ao_k_height_prev; +static ao_k_t ao_k_speed_prev; + +/* + * While in pad mode without a barometric sensor, remove accumulated + * speed and height values to reduce the effect of systematic sensor + * error + */ +void +ao_kalman_reset_accumulate(void) +{ + ao_k_height -= ao_k_height_prev; + ao_k_speed -= ao_k_speed_prev; + ao_k_height_prev = ao_k_height; + ao_k_speed_prev = ao_k_speed; +} +#endif + void ao_kalman(void) { ao_kalman_predict(); +#if HAS_BARO #if HAS_ACCEL if (ao_flight_state <= ao_flight_coast) { #ifdef FORCE_ACCEL @@ -283,12 +309,21 @@ ao_kalman(void) } else #endif ao_kalman_correct_baro(); +#else +#if HAS_ACCEL + ao_kalman_correct_accel(); +#endif +#endif ao_height = from_fix(ao_k_height); ao_speed = from_fix(ao_k_speed); ao_accel = from_fix(ao_k_accel); if (ao_height > ao_max_height) ao_max_height = ao_height; +#if HAS_BARO ao_avg_height_scaled = ao_avg_height_scaled - ao_avg_height + ao_sample_height; +#else + ao_avg_height_scaled = ao_avg_height_scaled - ao_avg_height + ao_height; +#endif #ifdef AO_FLIGHT_TEST if ((int16_t) (ao_sample_tick - ao_sample_prev_tick) > 50) ao_avg_height = (ao_avg_height_scaled + 1) >> 1;