X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=src%2Fkernel%2Fao_sample.c;h=9cba36c1004b37ec31717e7c4431e08ede4bf615;hb=HEAD;hp=e3b5e084d8f4c52ec454e30739910bfada8a9912;hpb=7f46240dfc57164f0c1b0c4c4ed9695bca63860d;p=fw%2Faltos

diff --git a/src/kernel/ao_sample.c b/src/kernel/ao_sample.c
index e3b5e084..422ccec6 100644
--- a/src/kernel/ao_sample.c
+++ b/src/kernel/ao_sample.c
@@ -21,6 +21,10 @@
 #include <ao_data.h>
 #endif
 
+#ifndef HAS_KALMAN
+#define HAS_KALMAN 1
+#endif
+
 #if HAS_GYRO
 #include <ao_quaternion.h>
 #endif
@@ -57,7 +61,7 @@ angle_t		ao_sample_orient;
 angle_t		ao_sample_orients[AO_NUM_ORIENT];
 uint8_t		ao_sample_orient_pos;
 #endif
-#ifdef HAS_MOTOR_PRESSURE
+#if HAS_MOTOR_PRESSURE
 motor_pressure_t	ao_sample_motor_pressure;
 #endif
 
@@ -161,7 +165,7 @@ static void
 ao_sample_set_one_orient(void)
 {
 	ao_sample_orients[ao_sample_orient_pos] = ao_sample_orient;
-	ao_sample_orient_pos = (ao_sample_orient_pos + 1) % AO_NUM_ORIENT;
+	ao_sample_orient_pos = (uint8_t) ((ao_sample_orient_pos + 1) % AO_NUM_ORIENT);
 }
 
 static void
@@ -190,7 +194,7 @@ ao_sample_compute_orient(void)
 	float rotz;
 	rotz = ao_rotation.z * ao_rotation.z - ao_rotation.y * ao_rotation.y - ao_rotation.x * ao_rotation.x + ao_rotation.r * ao_rotation.r;
 
-	ao_sample_orient = acosf(rotz) * (float) (180.0/M_PI);
+	ao_sample_orient = (angle_t) (acosf(rotz) * (float) (180.0/M_PI));
 }
 #endif /* HAS_GYRO */
 
@@ -198,7 +202,7 @@ static void
 ao_sample_preflight_set(void)
 {
 #if HAS_ACCEL
-	ao_ground_accel = ao_sample_accel_sum >> 9;
+	ao_ground_accel = (accel_t) (ao_sample_accel_sum >> 9);
 	ao_sample_accel_sum = 0;
 #endif
 #if HAS_BARO
@@ -207,15 +211,15 @@ ao_sample_preflight_set(void)
 	ao_sample_pres_sum = 0;
 #endif
 #if HAS_IMU
-	ao_ground_accel_along = ao_sample_accel_along_sum >> 9;
-	ao_ground_accel_across = ao_sample_accel_across_sum >> 9;
-	ao_ground_accel_through = ao_sample_accel_through_sum >> 9;
+	ao_ground_accel_along = (accel_t) (ao_sample_accel_along_sum >> 9);
+	ao_ground_accel_across = (accel_t) (ao_sample_accel_across_sum >> 9);
+	ao_ground_accel_through = (accel_t) (ao_sample_accel_through_sum >> 9);
 	ao_sample_accel_along_sum = 0;
 	ao_sample_accel_across_sum = 0;
 	ao_sample_accel_through_sum = 0;
 #endif
 #if HAS_MOTOR_PRESSURE
-	ao_ground_motor_pressure = ao_sample_motor_pressure_sum >> 9;
+	ao_ground_motor_pressure = (motor_pressure_t) (ao_sample_motor_pressure_sum >> 9);
 	ao_sample_motor_pressure_sum = 0;
 #endif
 #if HAS_GYRO
@@ -340,7 +344,7 @@ ao_sample_preflight_update(void)
 		++nsamples;
 	else
 		ao_sample_preflight_set();
-#if !HAS_BARO
+#if !HAS_BARO && HAS_KALMAN
 	if ((nsamples & 0x3f) == 0)
 		ao_kalman_reset_accumulate();
 #endif
@@ -406,7 +410,9 @@ ao_sample(void)
 		else {
 			if (ao_flight_state < ao_flight_boost)
 				ao_sample_preflight_update();
+#if HAS_KALMAN
 			ao_kalman();
+#endif
 #if HAS_GYRO
 			ao_sample_rotate();
 #endif