Dictionary:
gy·ro·com·pass (jī'rō-kŭm'pəs, -kŏm'-) ![]() |
| 5min Related Video: gyrocompass |
| Sci-Tech Encyclopedia: Gyrocompass |
A north-seeking form of gyroscope used as a directional reference in navigation. Modern gyrocompasses are so reliable and so much more accurate than magnetic compasses that they are now used as the prime navigational instrument on nearly every ship and on major aircraft and missiles. See also Magnetic compass.
A gyrocompass combines the action of two devices, a pendulum and a gyroscope, to produce alignment with the Earth's spin axis. The principle is demonstrated with the model shown in the illustration, which consists of a rapidly spinning, heavy gyro rotor, a pendulous case which permits the rotor axle to nod up and down (angle θ), and an outer gimbal which permits the axle to rotate in azimuth (angle ψ). For a gyroscope positioned at the Equator of the Earth, as the Earth rotates, the gimbal moves with it. So long as the rotor's spin axis is aligned with the Earth's axis, the gyro experiences no torque from Earth rotation. If there is misalignment, however, a sequence of restoring torques is initiated. See also Gyroscope; Pendulum.

Gyrocompass model.
In a shipboard installation the system must be mounted in a complete set of gimbals to isolate it from rolling, pitching, and yawing motions of the ship. Friction must be minimized. Moreover, Schuler tuning is employed to keep horizontal accelerations of the ship from producing false torques on the pendulum; the unique combination of gyro spin speed and pendulosity is chose so that no acceleration of the instrument can disturb its vertical reference. See also Schuler pendulum.
For many years the use of gyrocompasses in aircraft was impractical because of their high speed and large, rapid changes in attitude. The north-south component of vehicle velocity produces an error which depends on the velocity magnitude. Aircraft applications of gyrocompasses therefore use a modified version of the marine gyrocompass. The gyroscopes are mounted on a platform that is stabilized by signals from the gyroscopes. The platform is aligned to the local vertical and to north prior to takeoff by using essentially the same technique as for a marine gyrocompass. The 84-min Schuler period is shortened by amplifying signals from tilt sensors or accelerometers on the platform to rapidly remove platform tilt and align to north. Alignment times range from 5 to 30 min, depending upon the desired accuracy. The heading and vertical, once established, are “remembered” by the gyroscopes during flight. Vehicle velocity can be computed from the accelerometer data and used to correct for vehicle velocity and for dead-reckoning navigation. The need for preflight heading and vertical alignment can be eliminated by “gyrocompassing” this system in-flight by using an independent velocity sensorsuch as a Doppler radar. See also Doppler radar; Inertial guidance system.
| US Military Dictionary: gyrocompass |
n. a nonmagnetic compass in which the direction of true north is maintained by a continuously driven gyroscope whose axis is parallel to the earth's axis of rotation.
See the Introduction, Abbreviations and Pronunciation for further details.
| WordNet: gyrocompass |
The noun has one meaning:
Meaning #1:
a compass that does not depend on magnetism but uses a gyroscope instead
| Wikipedia: Gyrocompass |
A gyrocompass is similar to a gyroscope. It is a compass that finds true north by using an (electrically powered) fast-spinning wheel and friction forces in order to exploit the rotation of the Earth. Gyrocompasses are widely used on ships. They have two main advantages over magnetic compasses:
Contents |
A gyrocompass is essentially a gyroscope, a spinning wheel mounted on gimbals so that the wheel's axis is free to orient itself in any way. Suppose it is spun up to speed with its axis pointing in some direction other than the celestial pole. Because of the law of conservation of angular momentum, such a wheel will maintain its original orientation. Since the Earth rotates, it appears to a stationary observer on Earth that a gyroscope's axis is rotating once every 24 hours. Such a rotating gyroscope cannot be used for navigation. The crucial additional ingredient needed for a gyrocompass is some mechanism that results in applied torque whenever the compass's axis is not pointing north.
One method uses friction to apply the needed torque: the gyroscope in a gyrocompass is not completely free to reorient itself; if for instance a device connected to the axis is immersed in a viscous fluid, then that fluid will resist reorientation of the axis. This friction force caused by the fluid results in a torque acting on the axis, causing the axis to turn in a direction orthogonal to the torque (that is, to precess) towards the north celestial pole (approximately toward the North Star). Once the axis points toward the celestial pole, it will appear to be stationary and won't experience any more frictional forces. This is because true north is the only direction for which the gyroscope can remain on the surface of the earth and not be required to change. This is considered to be a point of minimum potential energy.
Another, more practical, method is to use weights to force the axis of the compass to remain horizontal with respect to the Earth's surface, but otherwise allow it to rotate freely within that plane. In this case, gravity will apply a torque forcing the compass's axis toward true north. Because the weights will confine the compass's axis to be horizontal with respect to the Earth's surface, the axis can never align with the Earth's axis (except on the Equator) and must realign itself as the Earth rotates. But with respect to the Earth's surface, the compass will appear to be stationary and pointing along the Earth's surface toward the true North Pole.
Since the operation of a gyrocompass crucially depends on the rotation of the Earth, it won't function correctly if the vessel it is mounted on is moving fast in an east to west direction.
The gyrocompass was patented in 1885 by the Dutch Marinus Gerardus van den Bos; however, his device never worked properly. In 1889, Captain Arthur Krebs designed an electric pendular gyroscope for the experimental French submarine Gymnote. It allowed the Gymnote to force a naval blockade in 1890. In 1903, the German Hermann Anschütz-Kaempfe (Raytheon Anschütz GmbH) constructed a working gyrocompass and obtained a patent on the design. In 1908, Anschütz-Kaempfe and the American inventor Elmer Ambrose Sperry patented the gyrocompass in Germany and the US. When Sperry attempted to sell this device to the German navy in 1914, Anschütz-Kaempfe sued for patent infringement. Sperry argued that Anschütz-Kaempfe's patent was invalid because it did not significantly improve on the earlier van den Bos patent. Albert Einstein testified in the case, first agreeing with Sperry but then reversing himself and finding that Anschütz-Kaempfe's patent was valid and that Sperry had infringed by using a specific damping method. Anschütz-Kaempfe won the case in 1915.
The gyrocompass can be subject to certain errors. These include steaming error, where rapid changes in course, speed and latitude cause deviation before the gyro can adjust itself.[1] On most modern ships the GPS or other navigational aids feed into the Gyrocompass allowing a small computer to apply a correction. Alternatively a design based on an orthogonal triad of fibre optic or ring laser gyroscopes will eliminate these errors as they depend upon no mechanical parts, instead using the principles of optical path difference to determine rate of rotation.[2]
This entry is from Wikipedia, the leading user-contributed encyclopedia. It may not have been reviewed by professional editors (see full disclaimer)
| gyro | |
| gyrocompass alignment (navigation) | |
| gyro |
| What are the scope and limitations of gyrocompass? | |
| What is the diffference between a gyrocompass and magnetic compass? | |
| What is the result of Gyrocompass near the poles? |
Copyrights:
![]() | Dictionary. The American Heritage® Dictionary of the English Language, Fourth Edition Copyright © 2007, 2000 by Houghton Mifflin Company. Updated in 2009. Published by Houghton Mifflin Company. All rights reserved. Read more | |
![]() | Sci-Tech Encyclopedia. McGraw-Hill Encyclopedia of Science and Technology. Copyright © 2005 by The McGraw-Hill Companies, Inc. All rights reserved. Read more | |
![]() | US Military Dictionary. The Oxford Essential Dictionary of the U.S. Military. Copyright © 2001, 2002 by Oxford University Press, Inc. All rights reserved. Read more | |
![]() | WordNet. WordNet 1.7.1 Copyright © 2001 by Princeton University. All rights reserved. Read more | |
![]() | Wikipedia. This article is licensed under the Creative Commons Attribution/Share-Alike License. It uses material from the Wikipedia article "Gyrocompass". Read more |
Mentioned in