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@ -647,7 +647,7 @@ FixedwingEstimator::start()
@@ -647,7 +647,7 @@ FixedwingEstimator::start()
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_estimator_task = task_spawn_cmd("fw_att_pos_estimator", |
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SCHED_DEFAULT, |
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SCHED_PRIORITY_MAX - 40, |
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12048, |
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6000, |
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(main_t)&FixedwingEstimator::task_main_trampoline, |
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nullptr); |
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@ -700,11 +700,11 @@ int fw_att_pos_estimator_main(int argc, char *argv[])
@@ -700,11 +700,11 @@ int fw_att_pos_estimator_main(int argc, char *argv[])
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math::EulerAngles euler(q); |
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printf("attitude: roll: %8.4f, pitch %8.4f, yaw: %8.4f degrees", |
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math::degrees(euler.getPhi()), math::degrees(euler.getTheta()), math::degrees(euler.getPsi())); |
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(double)math::degrees(euler.getPhi()), (double)math::degrees(euler.getTheta()), (double)math::degrees(euler.getPsi())); |
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printf("states [1-3]: %8.4f, %8.4f, %8.4f\n", states[0], states[1], states[2]); |
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printf("states [4-6]: %8.4f, %8.4f, %8.4f\n", states[3], states[4], states[5]); |
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printf("states [7-9]: %8.4f, %8.4f, %8.4f\n", states[6], states[7], states[8]); |
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printf("states [1-3]: %8.4f, %8.4f, %8.4f\n", (double)states[0], (double)states[1], (double)states[2]); |
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printf("states [4-6]: %8.4f, %8.4f, %8.4f\n", (double)states[3], (double)states[4], (double)states[5]); |
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printf("states [7-9]: %8.4f, %8.4f, %8.4f\n", (double)states[6], (double)states[7], (double)states[8]); |
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exit(0); |
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} else { |
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