ITU-R M 694-1-2005 Reference radiation pattern for ship earth station antennas《船上地球站天线的参考辐射类型》.pdf

1、 Rec. ITU-R M.694-1 1 RECOMMENDATION ITU-R M.694-1 Reference radiation pattern for ship earth station antennas (Question ITU-R 88/8) (1990-2005) Scope This Recommendation provides a reference radiation pattern for ship earth station antennas that should be used for coordination studies and the asses

2、sment of interference between ship earth stations in the mobile-satellite service (MSS) and terrestrial and space stations which share the same frequency bands. The technical considerations on the proposed reference radiation pattern are also contained in the Recommendation that include the existing

3、 reference radiation patterns used for various services, measured antenna patterns, and the effect of the reflection from the sea and a ships superstructure. The ITU Radiocommunication Assembly, considering a) that for coordination studies and the assessment of interference between ship earth statio

4、ns and terrestrial stations, and between ship earth stations and the space stations of different satellite systems sharing the same frequency bands, it may be appropriate to use a single radiation pattern for each type of ship earth station antenna; b) that the reference radiation pattern for ship e

5、arth station antennas must take account of the effect of local reflections from the sea, from a ships superstructure, etc.; c) that the use of antennas with the best achievable radiation pattern will lead to the most efficient use of the radio-frequency spectrum and the geostationary-satellite orbit

6、 recommends 1 that a single reference radiation pattern for each type of ship earth station antenna should be used for: 1.1 coordination studies and the assessment of interference between ship earth stations in the mobile-satellite service (MSS) and terrestrial stations in other services which shar

7、e the same frequency bands; 1.2 coordination studies and the assessment of interference between ship earth stations in the MSS and the space stations of different satellite systems which share the same frequency bands; 2 that the reference radiation pattern in Annex 1 should be used for ship earth s

8、tation antennas having circular paraboloidal reflectors with diameters between 0.8 m and 1.3 m and with an operating frequency range of 1518 to 1660.5 MHz; 3 that studies should continue in order to define the requirement for other types of ship earth station antennas. 2 Rec. ITU-R M.694-1 Annex 1 R

9、eference radiation pattern for ship earth station antennas having circular paraboloidal reflectors with diameters between 0.8 m and 1.3 m and with an operating frequency range of 1518 to 1660.5 MHz G = Gmax 2.5 103(D/ )2dB for 0 mG = 2 + 15 log (D/) dB for m 100 (/D) G = 52 10 log (D/) 25 log dB for

10、 100 (/D) 1G = 0 dB for 1 where: : angle from beam centre (degrees) m= 20 /D Gmax 2 15 log (D/) (degrees) 1= 120 (/D)0.4(degrees) G : gain of the antenna relative to isotropic (dB) Gmax: maximum gain of the antenna relative to isotropic (dB) unitsametheinexpressedwavelength :diameter antenna :DNOTE

11、1 The reference radiation pattern should be assumed to be rotationally symmetrical. Appendix 1 to this Annex provides the technical considerations on this reference radiation pattern, as demonstrated by some measured antenna patterns. Appendix 1 to Annex 1 Technical considerations on the reference r

12、adiation pattern for ship earth station antennas 1 Introduction This Appendix provides the technical considerations on the reference radiation pattern for ship earth station antennas in Annex 1. 2 Existing reference radiation patterns Reference radiation patterns have been studied and developed in v

13、arious Radiocommunication Study Groups. These study results provided a reference radiation pattern for antennas less than 100 , as stated below: Rec. ITU-R M.694-1 3 G = 52 10 log (D/) 25 log dB for 100 (/D) 1G = G1for 1 where: unitsametheinexpressedth waveleng:diameter antenna :D : angle from beam

14、centre (degrees). For values of less than 100 (/D), WARC-97 has defined the following reference radiation pattern for interference calculations: G = Gmax 2.5 103(D/ )2dB for 0 mG = 2 + 15 log (D/) dB for m 100 (/D) where: m= 20 /D Gmax 2 15 log (D/) (degrees) Gmax: maximum gain of the antenna relati

15、ve to isotropic. These equations assume the case of a circular paraboloidal reflector antenna, which might not be relevant for some kinds of antennas which could be used in the future for ship earth stations. Therefore, the use of this kind of pattern should clearly be restricted to the case of circ

16、ular paraboloidal reflector antennas. Moreover, the above reports have not specifically considered the question of the applicability of these equations to very small values of D/; therefore, for antennas of such diameter as small as 4 , the value of G1must be carefully established taking into accoun

17、t measured radiation patterns. 3 Measured antenna patterns All production designs of ship earth stations manufactured to date for use in the MARISAT system have employed a parabolic reflector antenna having a diameter of between 1.2 and 1.3 m with a G/T of 4 (dB(K1). This value is the current requir

18、ement for Inmarsat Standard-A ship earth stations. Figures 1 and 2 present the measured antenna pattern for a 1.3 m antenna for transmit and receive frequencies, respectively. Figures 3 and 4 present measured antenna patterns for a 1.2 m antenna for transmit and receive frequencies, respectively. Fi

19、gure 5 presents the measured antenna pattern for a 0.8 m antenna for receive frequencies. The reference radiation pattern in Annex 1 is included in all figures. With respect to the Inmarsat Standard-A ship earth stations, the following expression has been determined as the performance requirement fo

20、r the side-lobe envelope based on the measured radiation patterns of paraboloidal antenna with diameters between 0.8 m and 1.2 m: G = 8 dB for 16 21 G = 41 25 log dB for 21 57 G = 3 dB for 57 where G is the antenna gain relative to isotropic at an angle from beam centre. Figure 6 illustrates the Inm

21、arsat antenna pattern together with the reference radiation pattern derived from Annex 1 for a 1.2 m antenna diameter (24 dB maximum gain). 4 Rec. ITU-R M.694-1 FIGURE 1 Measured antenna pattern for a ship earth station antenna Type of antenna: circular parabolic Frequency band: 1 636.5-1 645 MHz (t

22、ransmit) Diameter: 1.3 m Rec. ITU-R M.694-1 5 FIGURE 2 Measured antenna pattern for a ship earth station antenna Type of antenna: circular parabolic Frequency band: 1 535-1 543.5 MHz (receive) Diameter: 1.3 m 6 Rec. ITU-R M.694-1 FIGURE 3 Measured antenna pattern for a ship earth station antenna Typ

23、e of antenna: circular parabolic Frequency band: 1 636.5-1 645 MHz (transmit) Diameter: 1.2 m Rec. ITU-R M.694-1 7 FIGURE 4 Measured antenna pattern for a ship earth station antenna Type of antenna: circular parabolic Frequency band: 1 535-1-1 543.5 MHz (receive) Diameter: 1.2 m 8 Rec. ITU-R M.694-1

24、 FIGURE 5 Measured antenna pattern of a ship earth station antenna Type of antenna: circular parabolic Frequency band: 1 535-1-1 543.5 MHz (receive) Diameter: 0.8 m Rec. ITU-R M.694-1 9 10 Rec. ITU-R M.694-1 4 The effect of reflection due to the sea and a ships superstructure Considerations have bee

25、n given to the concept that the design objectives and the reference radiation pattern for interference studies may be defined separately, because the reference radiation pattern should include the effect of local reflections from the sea and a ships superstructure. However, it is very difficult to e

26、stimate quantitatively such effects, which may be of the order of several dB, because the directions of reflected waves vary in accordance with the ships movement. Moreover, the time probability of the interference caused by such reflected side-lobes is very difficult to assess. Further study is needed to clarify the effect of such reflections.