测绘工程专业英语:Section 6 Determination of True Bearing by Gyro-thodolite.docx
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1、Section 6 Determination of True Bearing by Gyro-thodoliteThe gyroscope has been used in navigation as a north-seeking device for a considerable period of time and certain manufacturers of surveying instruments are now producing units which allow the direct establishment of the meridian by theodolite
2、 without the need for calculations based on astronomical observations.The development of the gyroscope for the precise transfer of bearings underground in mining surveying dates from about the beginning of the First World War, but an instrument capable of registering bearings to within one minute of
3、 arc did not appear until after the end of the Second World War. Even then i( was of considerable weight, but advances in the design of gyroscopes for airborne inertial navigation systems have allowed much more compact and portable units. For instance the Wild GAKI, described later, has a total mass
4、 of about 13.6kg, and its accuracy is of the same order as that obtained in sun observations.In this instrument a rotor or spinner is driven at speeds in excess of 20 0(X) rev/min, the axis of spin being in a horizontal- plane. Figure 1 shows the earth rotating about its axis with an angular velocit
5、y of at a place in latitude an angular velocity of 3cos 6 obtains about the meridian. The spinner of a gyroscope set up at this point will try (o maintain its initial spatial position provided that its angular momentum, L, is large, but the rotation of the earth itself pulls the spinner out of this
6、plane. There is a consequent reaction in the form of a rotation, or precession, about the vertical (or output) axis of the spinner which holds until the spin axis lies in the meridian at the place. Figure 2(a) shows the three axes of (he spinner and Fig. 2(b) shows the spin axis at an angle of a to
7、the meridian. The earths rotation causes an interference torque (Me) equal to L 3cos 0, and a consequent precessional couple of Me sin a is induced which forces the spinner into the meridian with an angular rate of 3cos 6 sin a. When the spinner is suspended (as it is in the GAK1 attachment) it will
8、 he seen that the maximum precessional couple occurs when is zero, i.e. at the equator, and that the gyro will float freely at the poles where cos 6 is zero. The precessing gyro does not align immediately on the meridian but oscillates about it.This can be placed on instruments such as Wild TIA, T16
9、 or T2 theodolites which must be suitably modified, and it is then connected (o a control unit or converter. The oscillating system (Fig. 3(a), containing the spinner and optical system with an index mark is carried by a tape suspended vertically within the chimney of the supporting case and fastene
10、d at the top. The converter contains a nickel-cadmium battery and an electronic unit; the battery is connected by leads to a six-way adaptor on the supporting case, and is controlled by a selector switch. A further switch indicating Yun and brake is provided with two indicators, one of which, measur
11、e*, shows a green colour when the spinner is revolving at its working speed. When setting up, the theodolite telescope should be roughly pointed towards north by means of, say, prismatic compass or tubular compass observations, and the gyro attachment can then be fastened on the theodolite with the
12、telescope in the face-left position. The cable from the converter unit is attached and the observer checks that the gyro is clamped by means of a device underneath the supporting case. The battery switch is set to on and when the other switch is set to run the wait indicator remains red for a short
13、period of time before the green color shows at measure, indicating that the spinner is now running at its correct operational speed and that it can be undamped. As the spinner oscillates about the meridian (he gyro index mark can be seen moving across an auxiliary scale in an observation tube, and w
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