mirror of https://github.com/ArduPilot/ardupilot
SITL: fix balancebot yaw reset to be kinimatically consistent
... or at least closer to it. We were hard-resetting the yaw to zero when the vehicle was upright. That makes for huge simulated gyro rates, and that means the differences between the gyros can be huge sample-to-sample, so we can get gyros-inconsistent errors. Fix things so we don't reset yaw at the same time as pitch, and also twist the vehicle to point North again when disarmed.
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@ -85,7 +85,7 @@ void BalanceBot::update(const struct sitl_input &input)
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const float delta_time = frame_time_us * 1.0e-6f;
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// yaw rate in degrees/s
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const float yaw_rate = calc_yaw_rate(steering);
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float yaw_rate = calc_yaw_rate(steering);
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// obtain roll, pitch, yaw from dcm
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float r, p, y;
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@ -98,6 +98,11 @@ void BalanceBot::update(const struct sitl_input &input)
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const float p_gain = 200;
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const float pitch_response = -sin(p) * p_gain * delta_time;
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ang_vel += pitch_response;
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// simulated fingers rotating the vehicle
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const float y_gain = 100000;
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const float yaw_response = -sin(wrap_180(y)) * y_gain * delta_time;
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yaw_rate += yaw_response;
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}
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// t1,t2,t3 are terms in the equation to find vehicle frame x acceleration
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@ -143,11 +148,15 @@ void BalanceBot::update(const struct sitl_input &input)
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// reset to vertical when not armed for faster testing
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accel_earth.zero();
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velocity_ef.zero();
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dcm.identity();
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gyro.zero();
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velocity_vf_x =0;
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gyro[1] = 0; // no pitch rate
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if (y < radians(2)) {
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// no rates at all:
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dcm.identity();
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gyro.zero();
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}
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}
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// work out acceleration as seen by the accelerometers. It sees the kinematic
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// acceleration (ie. real movement), plus gravity
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accel_body += dcm.transposed() * (Vector3f(0, 0, -GRAVITY_MSS));
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