1. A measuring method for analyzing the propagation of components of electromagnetic navigation signals,
wherein at least one representative transmitting unit is assigned to each navigation signal component, resulting in a plurality of transmitting units,
wherein an analysis unit is coupled to a receiving unit and carries out an amplitude detection at a first frequency, characterized in that the multiple representative transmitting units are operated offset in time without time overlap,
wherein every representative transmitting unit of the plurality of transmitting units is assigned a characteristic transmission-free leader pause duration andor transmission-free trailer pause duration for each of its assigned navigation signal components, which is respectively maintained between operating phases of the representative transmitting units,
wherein the analysis unit carries out a time-dependent amplitude detection,
wherein a time curve of received amplitude values is analyzed by the analysis unit to assign the representative transmitting unit and the assigned navigation signal components to timeslots of the received amplitude values, in that the pause durations in the time curve of the amplitude values are assigned to the leader pause durations andor trailer pause durations of the representative transmitting unit.
2. The measuring method according to claim 1 , wherein the propagation of the electromagnetic navigation signal components is analyzed with the aid of the representative transmitting units in scaled measuring environments, wherein the scaled measuring environments are shrunken in relation to the original environments to be analyzed, and
wherein the representative transmitting units assigned to the navigation signal components are operated using scaled, higher frequencies.
3. The method according to claim 1, wherein, for the amplitude detection, received signals around the first frequency are first converted to a lower intermediate frequency before the amplitude analysis is performed.
4. The method according to claim 1, wherein the representative transmitting units are operated using an identical first frequency.
5. The method according to claim 1, wherein the representative transmitting units are operated at various frequencies, which lie within the bandwidth of the amplitude detection.
6. The method according to claim 1 , wherein a plurality of representative transmitting units along a variable emission front is assigned to at least one navigation signal component, to simulate a position change or movement of the navigation signal components.
7. The method according to claim 1, wherein at least two of the representative transmitting units are oriented for emission in different spatial directions.
8. The method according to claim 1, wherein at least two sequential pause durations andor signal receiving durations in the amplitude values are analyzed by the analysis unit to assign the representative transmitting units to timeslots of the received amplitude values.
9. The method according to claim 1, wherein the representative transmitting units emit signals in the gigahertz range.
10. The method according to claim 1, wherein the amplitude detection occurs in the zero span mode of the analysis unit.
11. The method according to claim 1, wherein either active transmitting durations of the representative transmitting units or pause durations of the representative transmitting units are equal.
12. The method according to claim 1, wherein the chronological activation of the representative transmitting units is performed using HF switches andor delay lines.
13. The method according to claim 1, wherein the analysis unit is additionally implemented to analyze the frequency of received signals, in particular to detect Doppler shifts on the signal path.
14. A measuring method for analyzing the propagation of components of electromagnetic navigation signals,
wherein at least one representative transmitting unit is assigned to each navigation signal component, resulting in a plurality of transmitting units,
wherein an analysis unit is coupled to a receiving unit and carries out an amplitude detection at a first frequency, characterized in that the multiple representative transmitting units are operated offset in time without time overlap,
wherein each representative transmitting unit of the plurality of transmitting units is assigned a characteristic transmitting duration for each of its assigned navigation signal components, which is respectively maintained in operating phases of the representative transmitting units,
wherein the analysis unit carries out a time-dependent amplitude detection,
wherein a time curve of received amplitude values is analyzed by the analysis unit to assign the representative transmitting unit and the assigned navigation signal components to timeslots of the received amplitude values, in that the durations of the received signals in the time curve of amplitude values are assigned to the transmitting durations of the representative transmitting unit.
15. The measuring method according to claim 14, wherein the propagation of the electromagnetic navigation signal components is analyzed with the aid of the representative transmitting units in scaled measuring environments, wherein the scaled measuring environments are shrunken in relation to the original environments to be analyzed, and
wherein the representative transmitting units assigned to the navigation signal components are operated using scaled, higher frequencies.
16. The method according to claim 15, wherein at least one representative transmitting unit is fed using various chronological feed schemes, wherein the coupling of the feed is performed in a different manner for each of the feed schemes.
17. The method according to claim 14, wherein, for the amplitude detection, received signals around the first frequency are first converted to a lower intermediate frequency before the amplitude analysis is performed.
18. The method according to claim 14, wherein the representative transmitting units are operated using an identical first frequency.
19. The method according to claim 14, wherein the representative transmitting units are operated at various frequencies, which lie within the bandwidth of the amplitude detection.
20. The method according to claim 14, wherein at least one representative transmitting unit is fed using various chronological feed schemes, wherein the coupling of the feed is performed in a different manner for each of the feed schemes.
21. The method according to claim 14, wherein a plurality of representative transmitting units along a variable emission front is assigned to at least one navigation signal, to simulate a position change or movement of the navigation signal components.
22. The method according to claim 14, wherein at least two of the representative transmitting units are oriented for emission in different spatial directions.
23. The method according to claim 14, wherein at least two sequential pause durations andor signal receiving durations in the amplitude values are analyzed by the analysis unit to assign the representative transmitting units to timeslots of the received amplitude values.
24. The method according to claim 14, wherein the representative transmitting units emit signals in the gigahertz range.
25. The method according to claim 14, wherein the amplitude detection occurs in the zero span mode of the analysis unit.
26. The method according to claim 14, wherein either active transmitting durations of the representative transmitting units or pause durations of the representative transmitting units are equal.
27. The method according to claim 14, wherein the chronological activation of the representative transmitting units is performed using HF switches andor delay lines.
28. The method according to claim 14, wherein the analysis unit is additionally implemented to analyze the frequency of received signals, in particular to detect Doppler shifts on the signal path.
The claims below are in addition to those above.
All refrences to claim(s) which appear below refer to the numbering after this setence.
1. A telescopic sight comprising:
a main tube;
a reticule;
a reticule adjusting device arranged on the main tube for adjusting the reticule;
an optical focusing device and
a focus adjusting device arranged on the main tube for focusing the optical focusing device,
wherein the reticule adjusting device and the focus adjusting device are arranged so as to jointly form of an integrated adjusting device on the main tube.
2. The telescopic sight according to claim 1, wherein the integrated adjusting device is an integrated adjusting turret.
3. The telescopic sight according to claim 1, wherein at least one of the devices selected from the group consisting of the reticule adjusting device and the focus adjusting device has a rotatable or pivotable actuating element.
4. The telescopic sight according to claim 3, wherein the rotatable or pivotable actuating element is configured to be actuatable by hand.
5. The telescopic sight according to claim 3, wherein each of the reticule adjusting device and the focus adjusting device has a rotatable or pivotable actuating element, and the rotatable or pivotable actuating element of the reticule adjusting device is arranged substantially coaxially with the rotatable or pivotable actuating element of the focus adjusting device.
6. The telescopic sight according to claim 3, wherein the rotatable or pivotable actuating element is a rotary knob or a rotary ring.
7. The telescopic sight according to claim 3, wherein each of the reticule adjusting device and the focus adjusting device has a rotatable or pivotable actuating element, and the rotatable or pivotable actuating element of the reticule adjusting device is a rotary knob and the rotatable or pivotable actuating element of the focus adjusting device is a rotary ring.
8. The telescopic sight according to claim 7, wherein the rotary ring surrounds the rotary knob.
9. The telescopic sight according to claim 7, wherein the reticule adjusting device for adjusting the reticule has a spindle which is axially displaceable by rotation.
10. The telescopic sight according to claim 7, wherein the focus adjusting device has an inner ring mounted eccentrically in the rotary ring for converting a rotary movement into a linear movement.
11. The telescopic sight according to claim 1, wherein the reticule adjusting device is configured for at least one adjustment selected from a group consisting of a height adjustment and a lateral adjustment of the reticule.
12. The telescopic sight according to claim 1, wherein the reticule adjusting device and the focus adjusting device are capable of being coupled for automatic ballistic correction.
13. The telescopic sight according to claim 1, wherein the main tube has a central tube arranged between an objective lens region and an eyepiece region and the integrated adjusting device is arranged in the region of the central tube.
14. The telescopic sight according to claim 13, wherein at least one region selected from a group consisting of an objective lens region of the main tube and an eyepiece region of the main tube has a larger diameter than the central tube.
15. The telescopic sight according to claim 1, wherein the integrated adjusting device is arranged on the top on the main tube in an operative position of the telescopic sight.
16. The telescopic sight according to claim 1, wherein the reticule is integrated into a reversal system of the telescopic sight.
17. The telescopic sight according to claim 1, wherein the reticule adjusting device and the focus adjusting device are arranged in a combined adjusting device which is fixed on the main tube.