A set of three orthogonally aligned torque rods wired up so they can generate a magnetic dipole field of either sign (i.e. flip the North and South. Magnetic Torquers. These devices interact with the Earth’s magnetic field and create control torque, which can be adjusted to the required value. Combined with. In this work the issue of acceleration disturbances onboard of GRACE due to magnetic torquers is investigated and discussed. Each of the.

Author: Kecage Vudora
Country: Lithuania
Language: English (Spanish)
Genre: Business
Published (Last): 16 May 2017
Pages: 328
PDF File Size: 13.14 Mb
ePub File Size: 15.19 Mb
ISBN: 583-7-69812-978-4
Downloads: 40498
Price: Free* [*Free Regsitration Required]
Uploader: Guzragore

A broader disadvantage is the dependence on Earth’s magnetic field strength, making this approach unsuitable for deep space missions, and also more suitable for low Earth orbits as opposed to higher ones like the geosynchronous. Essentially, what happens when you turn on the magnetorquer is that there is a torque applied to move the spacecraft to line up with the magnetic field vector. This means as the spacecraft orbits the Earth it encounters a diversity of Earth magnetic field orientations and in general the time-averaged effect of this field diversity enables full 3-axis control.

This artificial field interacts with the Earth’s magnetic field to produce a net external torque on the vehicle that will tend to line up the fields.

Subsequently, the torques provided are very limited and only serve to accelerate or decelerate the change in a spacecraft’s attitude by minute amounts.

That said, the field is weak, so the actual torque produced by torque rods is very small.

Magnetorquer – Wikipedia

Basically, most magnetorquers function something like bar magnets that can be dialed to select how powerful, and what direction, they pull in. The main disadvantage of magnetorquers is that very high magnetic flux densities are needed if large craft have to be turned very tirquers.

Proof of the ineffectiveness of torque rods in the absence of magnetic field diversity Torque rods rely on the change in direction of the Earth’s magnetic field, which is especially problematic in equatorial orbits because to first order the field has a constant inertial direction. Without resistance, it will overshoot the pole, making it difficult to exactly line up on an axis.

Mathematically, the torque is provided in the direction of: Archived from the original pdf on Over time active control can produce very fast spinning even here, but for accurate attitude control and stabilization the torques provided often aren’t enough. What is the math behind Magnetorquers? This makes it possible to freely pivot the craft around in a known local gradient of the magnetic field by torsuers using electrical energy.


We could have started at this step by choosing the principle reference frame to start, but many seem comforted by starting with the full EOM. There is always one axis that you cannot rotate about, although you might be able to mitigate it with some effort. However, there are different ways to obtain the coil, thus according to the construction strategy it is possible to find three type of magnetorquer, apparently very different from each other but based on the same concept [1]:.

Magnetorquers are essentially sets of electromagnets which are laid out to yield a rotationally asymmetric anisotropic magnetic field over an extended area. This page was last edited on 2 Decemberat From Wikipedia, the free encyclopedia. Equating the control torque with the rigid-body rotational equations of motion:. Magnetorquers are lightweight, reliable, and energy-efficient.

Adam Wuerl 3, 11 If you are lined up perfectly with the magnetic field, you cannot control your rotation about the field. Equating the control torque torqusrs the rigid-body rotational equations of motion: I know that even if you have 3 axis of magnetic torquers, in effect there is only 2 axis of control, and I’m trying to figure out how all of this works exactly. The magnetic dipole generated by the magnetorquer is expressed by the formula:. Typically three coils are used, although reduced configurations of two or even one magnet can suffice where full attitude control is not needed or external forces like asymmetric drag allow underactuated control.

artificial satellite – What is the math behind Magnetorquers? – Space Exploration Stack Exchange

It’s completely unsuitable for agile spacecraft e. Retrieved from ” https: However, remember that the magnetic field lines around the Earth are themselves a dipole field, which is a toroidal shape. The math behind them turns out to be really simple. Home Questions Tags Users Unanswered. By using our site, you acknowledge that you have read and understand our Cookie PolicyPrivacy Policyand our Terms of Service. By clicking “Post Your Answer”, you acknowledge that you have read our updated terms of serviceprivacy policy and cookie policyand that your continued use of the website is subject to these policies.



A further advantage over momentum wheels and control moment gyroscopes is the absence of moving parts and therefore significantly higher reliability.

Specifically, let’s assume the following hypothetical situation:. Post as a guest Name. The three coil assembly usually takes the form of three perpendicular coils, because this setup equalizes the rotational symmetry of the fields which can be generated; no matter how the external field magneitc the craft are placed with respect to each other, approximately the same torque can always be generated simply by using toorquers amounts of current on the three different coils.

It is also impossible to control attitude in all three axes even if the full three coils are used, because the torque can be generated only perpendicular to the Earth’s magnetic field vector. As long as current is passing through the coils and the spacecraft has not yet been stabilized in a fixed orientation with respect to the external field, the craft’s spinning will continue.

I have a location of a satellite in LEO, and the magnetic field vector for said satellite. All articles with unsourced statements Articles torwuers unsourced statements from November Articles with unsourced statements from December This torque only has two degrees mavnetic freedom, i.

Math is very frequently helpful in spaceflight. Spacecraft attitude control Spacecraft propulsion Spacecraft components.

Furthermore, one must consider that there are in effect only 2 axis of rotation. The magnets themselves are mechanically anchored to the craft, so that any magnetic force they exert on the surrounding magnetic field will lead to a magnetic reverse force and result in mechanical torque about the vessel’s center of gravity. The full analysis will be easier to apply by measuring one magnetorquer at a time, but I’m going to assume that their torque lines up with the rotational vectors reasonably well, allowing for all of them to be handled.