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Estimating attitude by fusing the sensors

1.[2p]

In the complementary filter θα(θ+ωΔt)+(1-α)θacc, the term multiplied by α is

Correct
The answer is: the integrated gyroscope, which is fast but would drift on its own
The answer is: the integrated gyroscope, which is fast but would drift on its own
The answer is: the integrated gyroscope, which is fast but would drift on its own

2.[2p]

The small (1-α) accelerometer term in the filter is there to

Correct
The answer is: nudge the estimate slowly toward true level and cancel the gyro's drift
The answer is: nudge the estimate slowly toward true level and cancel the gyro's drift
The answer is: nudge the estimate slowly toward true level and cancel the gyro's drift

3.[3p]

A complementary filter runs at Δt=0.001 s with α=0.98. Using τ=αΔt/(1-α), what is its time constant, in seconds, to three decimal places?

CorrectNot quite: 0.049

4.[2p]

The accelerometer cannot correct yaw drift because

Correct
The answer is: gravity points the same way whatever heading the craft faces, so it carries no heading information
The answer is: gravity points the same way whatever heading the craft faces, so it carries no heading information
The answer is: gravity points the same way whatever heading the craft faces, so it carries no heading information

5.[2p]

A magnetometer is added to a craft that must hold a heading because

Correct
The answer is: it reads the Earth's magnetic field to give an absolute heading, correcting the yaw drift
The answer is: it reads the Earth's magnetic field to give an absolute heading, correcting the yaw drift
The answer is: it reads the Earth's magnetic field to give an absolute heading, correcting the yaw drift

6.[2p]

Acrobatic flight controllers store attitude as a quaternion rather than three angles because

Correct
The answer is: three angles suffer gimbal lock at some orientations, while a quaternion never becomes singular
The answer is: three angles suffer gimbal lock at some orientations, while a quaternion never becomes singular
The answer is: three angles suffer gimbal lock at some orientations, while a quaternion never becomes singular

7.[2p]

A noisy or delayed attitude estimate can always be fixed by tuning the control loop harder downstream.

The answer is: False
Correct