13 PDF Article

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: Shaktilar Zulurg
Country: Denmark
Language: English (Spanish)
Genre: Travel
Published (Last): 2 September 2005
Pages: 358
PDF File Size: 20.46 Mb
ePub File Size: 7.9 Mb
ISBN: 709-4-48491-712-2
Downloads: 17234
Price: Free* [*Free Regsitration Required]
Uploader: Mazusho

Post as a guest Name. 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]:.

From Wikipedia, the free encyclopedia. Like a compass needle, the magnet will line magneric with the north pole of the magnet lining up to the south magnetic field.

How much control authority do I have, given a magnetic field in body coordinates, and 3 equal strength magnetorquers in orthogonal vectors lined up with the body axis? The magnetorquer creates a magnetic dipole that interfaces with an ambient magnetic field, usually Earth’sso that the counter-forces produced provide useful torque.

Torque rods are used to desaturate these effectors which accumulate momentum due to disturbance torques like atmospheric drag, and to de-spin satellites e. Email Required, but never shown.

Magnetic Torquer VMT – VECTRONIC Aerospace

This is not always possible within the energy constraints of the vessel. I have togquers location of a satellite in LEO, and the magnetic field vector for said satellite. What is the math behind Magnetorquers? 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.

Views Read Edit View history. 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. By using this site, you agree to the Terms of Use and Privacy Policy.

A further advantage over momentum wheels and control moment gyroscopes is the absence of moving parts and therefore significantly higher reliability. Basically, most magnetorquers function something like bar magnets that can be dialed to magnetiic how powerful, and what direction, they pull in. Specifically, let’s assume the following hypothetical situation:. Equating the control torque with the rigid-body rotational equations of motion:. 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.


Spacecraft attitude control Spacecraft propulsion Spacecraft components.

This makes it possible to freely pivot the craft around in a known local gradient of the magnetic field by only using electrical energy. 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.

Equating the control torque with the rigid-body rotational equations of motion: That said, the field is weak, so the actual torque produced by torque rods is very small. A set of three orthogonally aligned torque rods wired up so they can generate a magnetic dipole field of either sign i. The dependence on the highly variable intensity of Earth’s magnetic field is also problematic because then the attitude control problem becomes highly nonlinear.

Magnetorquers are lightweight, reliable, and energy-efficient. In Earth orbit, sunlight is one such practically inexhaustible energy source, using solar panels. 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.

A magnetorquer or magnetic torquer also known as torque rod is a satellite system for attitude controldetumbling, and stabilization built from electromagnetic torqusrs. 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 magneitc Earth orbits as opposed to higher ones like the geosynchronous.

The construction of a magnetorquer is based on the realization of a coil with a defined area and number of turns according to the required performances. 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 torquuers result in mechanical torque about the vessel’s center of gravity.

All articles with unsourced statements Articles with unsourced statements from November Articles with unsourced statements from December It’s completely unsuitable for agile spacecraft e. The dipole interacts with the magnetic field generating a torque whose expression is:. Magnetorquers are essentially magetic 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 Furthermore, one must consider that there are in effect only 2 axis of rotation. 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. 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.

I know that even if you have 3 axis of magnetic torquers, in effect there is only 2 axis of control, and I’m torquesr to figure out how all of this works exactly. Any spinning satellite made of a conductive material will lose rotational momentum in Earth’s magnetic field due to generation of eddy currents in its body and the corresponding braking force proportional to its spin rate. 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.

Mathematically, the torque is provided in the direction of:. 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: Very small satellites may use permanent magnets instead of magneic.

Sign up using Facebook. By using our site, you acknowledge that you amgnetic read and understand our Cookie PolicyPrivacy Policyand our Terms of Service. Adam Wuerl 3, 11 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.

Magnetic Torquer VMT-35

The math behind them turns out to be really simple. The maynetic dipole generated by the magnetorquer is expressed by the formula:. The main disadvantage of magnetorquers is that very high magnetic flux densities are needed if large craft have to be turned very fast. This either necessitates a very high current in the coils, or much higher ambient flux densities than are available in Earth orbit.