iii? w Fig. 2 explains the electronic part. It consists of a pulse generator and a control unit. The two corre sponding printed circuits are placed in a small box, that serves the following actions: start/stop, rota tion left/right, and speed regulation. The velocity of the star to be observed should be first adjusted on a calibrated scale and the movable wire set in the start position. When the star reaches the movable wire in the field of view, the observer starts the motor and keeps subsequently the movable wire in coincidence with the star. This is done by means of the large knob. In neutral position of this knob the wire moves with the nominal velocity of the star, turning the knob to the left the velocity decreases (min. 0), turning to the right the velocity increases (max. twice the nominal veloc ity). 3 Investigation of the motor-micrometer using an artificial star The accuracy of the motor-micrometer was investi gated using an artificial star as shown in Fig. 3. The star is simulated by an illuminated fine diaphragm mounted on a carriage. This carriage is moved by a synchronous motor via a wormgear over a range of about 0.5 meter. The direction of the motion is reversed automatically by microswitches at both ends of the rail of the carriage. In order to control the position of the artificial star, two reference points are selected near the ends of the star's path. When the star passes these reference points, an electric pulse is produced by a photocell, stable multi vibrator MOTOR GENERATOR CONTROL UNIT 92340 range fine Nominal velocity adjustment Velocity regulation Fig. 1. Kern DKM 3A with motor-micrometer. 1. step motor; 2. contra weight; 3. ocular; 4. nominal velocity adjustment; 5. direction of rotation: left/ right; 6. velocity regulation; 7. start/stop; 8. input 12 Volt D.C.; 9. on/off; 10. D.C. indicator; 11. con nector for the chronograph; 12. connector for step motor and mechanical contacts; 13. connector for frequency counter (calibration); 14. illumination; 15. resistance for illumination. Fig. 2. Block diagram of electronical part. Fig. 3. Artificial star 1. frame for guidance; 2. illuminated diaphragm; 3. synchronous motor and transmission; 4. disc with slit; 5. photocell; 6. photocell pulse indicator; 7. microswitch; 8. relay; 9. resistance for brightness ("magnitude"). 50 ngt 73

Digitale Tijdschriftenarchief Stichting De Hollandse Cirkel en Geo Informatie Nederland

Nederlands Geodetisch Tijdschrift (NGT) | 1973 | | pagina 12