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Wing Leveling Using Earth Magnetism

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ballensr

Aerospace
Dec 3, 2002
4
Dacades ago I read about experiments using the Earth's magnetic field to keep the wings level on a high altitude gas powered model airplane. It would seem to have application to today's UAVs our military is using in the Middle East.

Does anyone have knowledge on how to mechanize such a system?

W. D. Allen Sr.
ballensr@adelphia.net

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I can't imagine how this could work since the Earth's field is NEVER horizontal.
 
It's neither necessary nor practical.

The currently accepted means of measuring magnetic field for this type of application is a modification of a fluxgate compass, which has a basic accuracy no better than 0.1 deg.

The inertial nav system on a UAV such as Predator would be accurate to better than 0.001 deg.

Since the Earth's field can vary drastically over short distances, a fluxgate compass would need to be compensated, while the inertial nav system is immune to this.

TTFN

 
A tenth of a degree should be atisfactory for leveling the wings since the system probably measured the differential of gauss values at at the wing tips. Keeping the wings level as opposed to letting the plane slowly roll into a graveyard spiral was probably their intent, not precise navigation.

Thanks,

WDA
 
The fluxgate is only about 1" across. The fluxgate measures absolute magnetic orientation, but localized mass concentrations can throw it for a loop ;-)

The inertial attitude gyro is a mandatory requirement, and it tells you absolute roll relative to earth, so there is no need for any other roll indicator.

TTFN
 
A similar system was tried in the roll control of anti-tank missiles in the early 80's. The missile had a shaped charge that required to overfly the tank in the right roll orientation due to the effects of a spinning tail stability system. To do this, the missile emerged from the launch tube, took a magnetic "sounding" and used this as its roll datum. Any deviation (due to roll) caused an emf to be generated in a transverse mounted coil and core - the output of which was conditioned and used to operate roll control fins. This was, I believe, a purely comparative system.
 


wether it works on not, what do you plan to do when the poles flip or when you fly south over the poles?
 
Gauss measurement devices were placed in each wing tip and in the nose and tail of the fuselage of a model airplane. Differential measurements were taken to determine bank and pitch respectively to stabilize the attitude. This approach was used in an R/C powered airplane to set some kind of flight endurance record. Unfortunately that was a couple of decades ago and no reference data are readily available today.

A similar attitude control approach should work for today's military and civilian UAVs, precluding the need for attitude gyros.

WDA

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And what would tehn tell you that you were upside down?

TTFN
 
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