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Aircraft Flight Mechanics - M3L05: Air data vs IMU; relative motion
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Our aircraft air data system ain't in the origin of the body axes (else it wouldn't be able to measure *anything*), so how can we use it to get aircraft velocity? Furthermore, how can we use it get aircraft AoA and SS?
What if we damage some of the air data system, and have one of the measurements but not the other two. Can we use IMU (inertial measurement system) data to recover the other two? (Spoiler: we can).
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At about 31 minutes or so, I make a mistake in the W velocity - it should be +Qx_p, not minus. U and V are fine, but W is off by about 2m/s. The answers should be:
The a/c velocity components are U=37.50m/s, V=25.00m/s, W=24.27m/s
Giving a flightspeed of Vf=51.19m/s, and α=32.91deg, β=29.24deg
Which is actually pretty close to what I got, so I didn't catch it.
What if we damage some of the air data system, and have one of the measurements but not the other two. Can we use IMU (inertial measurement system) data to recover the other two? (Spoiler: we can).
------
At about 31 minutes or so, I make a mistake in the W velocity - it should be +Qx_p, not minus. U and V are fine, but W is off by about 2m/s. The answers should be:
The a/c velocity components are U=37.50m/s, V=25.00m/s, W=24.27m/s
Giving a flightspeed of Vf=51.19m/s, and α=32.91deg, β=29.24deg
Which is actually pretty close to what I got, so I didn't catch it.
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