Aircraft guidance question: Effect of mounting sensors at the CG vs on the Tail

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SUMMARY

The discussion centers on the optimal placement of a magnetometer sensor on an airborne platform, specifically comparing mounting it at the center of gravity (CG) versus the tail. It is established that positioning the sensor at the CG minimizes the effects of amplified moments due to arm length, thereby enhancing stability and data accuracy. The conversation highlights the importance of maintaining sensor orientation and the role of various inertial navigation tools, including GPS, 3D accelerometers, and Kalman filters, in determining the sensor's effectiveness. The consensus is that while both positions have their merits, the CG offers significant advantages in terms of stability and reduced error susceptibility.

PREREQUISITES
  • Understanding of inertial navigation systems, including 3D accelerometers and gyros.
  • Familiarity with magnetometer functionality and its application in airborne platforms.
  • Knowledge of Kalman filtering techniques for data integration and error correction.
  • Basic principles of aerodynamics, particularly the concepts of center of gravity and center of pressure.
NEXT STEPS
  • Research the principles of inertial navigation and the role of 3D rate gyros in orientation determination.
  • Study the application of Kalman filters in sensor data fusion for improved accuracy.
  • Explore the effects of sensor placement on stability and error susceptibility in airborne systems.
  • Investigate the Brouwer fixed-point theorem and its relevance to sensor positioning in dynamic environments.
USEFUL FOR

Aerospace engineers, sensor integration specialists, and researchers in inertial navigation systems will benefit from this discussion, particularly those focused on optimizing sensor placement for enhanced stability and data accuracy in airborne applications.

cessna1525
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Hi,

Can I someone please explain to me, the moment behaviors of having something fixed on CG vs on Tail in a rocket? are there any benefits of having a Sensor on CG than fixed on the tail?

Thank you
 
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Welcome to PF.

Is the something, a linear accelerometer and rotational gyroscope, used for inertial navigation?

The CG will move as fuel is consumed. How will you move the something?

The tail will be where the data is needed to balance, steer, and stabilise the rocket.
 
Hi,
Thank you very much for the quick reply, actually. the case here is about an airborne Magnetometer bird, just wanted to know if there is any benefit of having the Mag sensor on CG instead of on the Tail section, The argument I heard from my colleague is Having on the CG is better because having it on the Tail section will cause amplified moments due to the arm, does this make sense? , I thought it doesnt matter like that
 
cessna1525 said:
the case here is about an airborne Magnetometer bird
Like this?

1688393178124.png

https://www.bgr.bund.de/EN/Themen/G...omagnetometrie/aeromagnetometrie_node_en.html
 
Yes, exactly, only difference is we are hanging it on one point, just above the CG,
 
cessna1525 said:
Yes, exactly, only difference is we are hanging it on one point, just above the CG,
How do you keep the sensor body horizontal if you only support it at the CG?
 
It is balanced on the CG , and CG is Infront of the Center of pressure, and it stabilized as it speeds up, usually 15 m/s forward speed.
 
cessna1525 said:
are there any benefits of having a Sensor on CG than fixed on the tail?
The orientation of the magnetometer will vary in the same way, independent of its position on the bird.

However, the distance of the magnetometer from the tow vehicle, and from the ground, will vary with the changing orientation of the bird, but will be minimised if the instrument is close to the centre of mass of the bird.
 
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Thank you so much for the input, is there any subject material on this which I could Study more?
what is the theory behind
 
  • #10
cessna1525 said:
what is the theory behind
When you stir a cup of tea, at every point in time, there is at least one point that is fixed in position. Likewise, when a magnetometer bird moves through the air, the centre of mass is probably near a virtual "fixed point" on the bird.
https://en.wikipedia.org/wiki/Brouwer_fixed-point_theorem

You have GPS, 3D accelerometers, 3D rate gyros, and a 3D magnetometer. Everything is fixed to the frame of the bird, but offset in different positions.

The orientation of the bird comes from the 3D rate gyros.
The long term track is determined by GPS. The short term track comes from the 3D accelerometers, corrected for orientation. The long and short term tracks are combined in a Kalman filter.
https://en.wikipedia.org/wiki/Kalman_filter

The position of the magnetometer is computed from the spatial track.
The orientation of the magnetic field is corrected for bird orientation.

The orientation of the bird is computed with quaternions to avoid gimbal-lock in the calculations.
https://en.wikipedia.org/wiki/Quaternion
https://en.wikipedia.org/wiki/Gimbal_lock

Transducers.
https://www.analog.com/en/technical...l-ways-to-assemble-mems-inertial-sensors.html
 
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  • #11
cessna1525 said:
It is balanced on the CG , and CG is Infront of the Center of pressure, and it stabilized as it speeds up, usually 15 m/s forward speed.
Choosing the place to put it could give a least worst susceptibility to error but would it not be necessary to apply corrections all the time?
In addition, won't yaw and the vertical axis of the centre of lateral pressure also be relevant? Centres of pressure will probably move about, in any case, as the device is pulled in different directions. I'd imagine that damping and stability would also be relevant - more than just choosing the placing wrt the centre of pressure.
 

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