Estimating attitude by fusing the sensors
1.[2p] In the complementary filter , the term multiplied by is
In the complementary filter , the term multiplied by 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 accelerometer term in the filter is there to
The small 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 s with . Using , what is its time constant, in seconds, to three decimal places?
A complementary filter runs at s with . Using , what is its time constant, in seconds, to three decimal places?
CorrectNot quite: 0.049
4.[2p] The accelerometer cannot correct yaw drift because
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
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
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.
A noisy or delayed attitude estimate can always be fixed by tuning the control loop harder downstream.
The answer is: False
Correct