ITU-R RS 1632-2003 Sharing in the band 5 250-5 350 MHz between the Earth exploration-satellite service (active) and wireless access systems (including radio local area networks) in.pdf
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1、 Rec. ITU-R RS.1632 1 RECOMMENDATION ITU-R RS.1632*Sharing in the band 5 250-5 350 MHz between the Earth exploration-satellite service (active) and wireless access systems (including radio local area networks) in the mobile service (Question ITU-R 218/7) (2003) The ITU Radiocommunication Assembly, c
2、onsidering a) that the frequency band 5 250-5 350 MHz is allocated to the Earth exploration-satellite service (EESS) (active) and to the radiolocation service on a primary basis; b) that some administrations have proposed to use the band 5 250-5 350 MHz for low power high speed wireless local area n
3、etworks (WLANs), or radio local area networks (RLANs); c) that these high speed WLANs are proposed to be deployed in the band as unlicensed devices, making regulatory control of their deployment density non-feasible, recognizing a) that studies are continuing in ITU-R with a view to facilitating sha
4、ring of wireless access systems (including RLANs) with EESS (active), noting a) that some administrations have adopted technical limits which permit wireless access systems (including RLANs) to operate with an e.i.r.p. power limit of l W, while other administrations have adopted more stringent e.i.r
5、.p. limits, recommends 1 that sharing between spaceborne active sensors of the EESS with the characteristics as given in Annex 1 and high speed WLANs in the 5 250-5 350 MHz band is feasible with wireless access systems (including RLANs) having constraints such as those given in Annex 2; 2 that the l
6、evel of protection required for EESS systems as given in Annex 1 may also be achieved using alternative sets of operational and technical limits being studies under recognizing a). *Radiocommunication Study Group 7 made editorial amendments to this Recommendation. 2 Rec. ITU-R RS.1632 Annex 1 Techni
7、cal characteristics of spaceborne active sensors in the 5 250-5 570 MHz band Technical characteristics of spaceborne active sensors in the 5.3 GHz frequency range are given in Tables 1 and 2. TABLE 1 5.3 GHz typical spaceborne imaging radar characteristics Value Parameter SAR1 SAR2 SAR3 SAR4 Orbital
8、 altitude (km) 426 (circular) 600 (circular) 400 (circular) 400 (circular) Orbital inclination (degrees) 57 57 57 57 RF centre frequency (MHz) 5 305 5 405 5 405 5 300 Peak radiated power (W) 4.8 4 800 1 700 1 700 Polarization Horizontal (HH) Horizontal and vertical (HH, HV, VH, VV) Horizontal and ve
9、rtical (HH, HV, VH, VV) Horizontal and vertical (HH, HV, VH, VV) Pulse modulation Linear FM chirp Linear FM chirp Linear FM chirp Linear FM chirp Pulse bandwidth (MHz) 8.5 310 310 40 Pulse duration (s) 100 31 33 33 Pulse repetition rate (pps) 650 4 492 1 395 1 395 Duty cycle (%) 6.5 13.9 5.9 5.9 Ran
10、ge compression ratio 850 9 610 10 230 1 320 Antenna type (m) Planar phased array 0.5 16.0 Planar phased array 1.8 3.8 Planar phased array 0.7 12.0 Planar phased array 0.7 12.0 Rec. ITU-R RS.1632 3 TABLE 1 (end) Value Parameter SAR1 SAR2 SAR3 SAR4 Antenna peak gain (dBi) 42.2 42.9 42.7/38 (full focus
11、/beamspoiling) 42.7/38 (full focus/beamspoiling) Antenna median side lobe gain (dBi) 5 5 5 5 Antenna orientation (degrees from nadir) 30 20-38 20-55 20-55 Antenna beamwidth (degrees) 8.5 (El), 0.25 (Az) 1.7 (El), 0.78 (Az) 4.9/18.0 (El), 0.25 (Az) 4.9/18.0 (El), 0.25 (Az) Antenna polarization Linear
12、 horizontal/vertical Linear horizontal/vertical Linear horizontal/vertical Linear horizontal/vertical Receiver front end 1 dB compression point ref to receiver input (dBW) 62 input 62 input 62 input 62 input Allowable density of configuration saturation ref to receiver input 114/54 dBW input at 71/1
13、1 dB receiver gain 114/54 dBW input at 71/11 dB receiver gain 114/54 dBW input at 71/11 dB receiver gain 114/54 dBW input at 71/11 dB receiver gain Receiver input max. power handling (dBW) +7 +7 +7 +7 Operating time (%) 30 the orbit 30 the orbit 30 the orbit 30 the orbit Minimum time for imaging (s)
14、 9 15 15 15 Service area Land masses and coastal areas Land masses and coastal areas Land masses and coastal areas Land masses and coastal areas Image swath width (km) 50 20 16/320 16/320 4 Rec. ITU-R RS.1632 TABLE 2 5.3 GHz typical spaceborne radar altimeter characteristics TABLE 3 5.3 GHz typical
15、spaceborne scatterometer characteristics Jason mission characteristics Lifetime 5 years Altitude 1 347 km 15 km Inclination 66 Poseidon 2 altimeter characteristics Signal type Pulsed chirp. linear FM C band pulse repetition frequency (PRF) 300 Hz Pulse duration 105.6 s Carrier frequency 5.3 GHz Band
16、width (BW) 320 MHz Emission RF peak power 17 W Emission RF mean power 0.54 W Antenna gain 32.2 dBi 3 dB aperture 3.4 Side lobe level/maximum 20 dB Backside lobe level/maximum 40 dB Beam footprint at 3 dB 77 km Interference threshold 118 dBW Parameter Value System name Scatterometer 1 Scatterometer 2
17、 Orbital altitude (km) 780 800 Inclination (degrees) 98.5 98.5 Centre frequency (GHz) 5.3 5.255 Pulse width 70 s (mid) 8 ms (mid) 130 s (fore/aft) 10.1 ms (fore/aft) Modulation Interrupted CW Linear FM (chirp) Transmitter BW (kHz) 15 500 PRF (Hz) 115 (mid) 29.4 98 (fore/aft) Antenna type Slotted wav
18、eguide Slotted waveguide Rec. ITU-R RS.1632 5 TABLE 3 (end) Annex 2 Sharing constraints between spaceborne active sensors and high speed WLANs in the 5 250-5 350 MHz band 1 Introduction This Annex presents the results of three sharing analyses for the band 5 250-5 350 MHz between the spaceborne acti
19、ve sensors and the high speed WLANs, or RLANs. The first study, given in 2 of this Annex, uses high performance RLAN (HIPERLAN) type 1 classes B and C and HIPERLAN type 2 characteristics for the RLANs and uses SAR4 characteristics for the SAR. In this study, it is feasible for the indoor only HIPERL
20、AN type 1 class B and HIPERLAN type 2 to share the 5 250-5 350 MHz band with SAR4, but is not feasible for the HIPERLAN type 1 class C to share the band, nor for any HIPERLAN type designed to be operated outdoors with the technical characteristics assumed in the study. The second study, as given in
21、3 of this Annex, uses three RLAN types, RLAN1, RLAN2, and RLAN3, and uses SAR2, SAR3, and SAR4 characteristics for the SARs. In this study, for the single transmitter deployed outdoors, the RLAN1 high speed WLAN transmitter interference was above the acceptable level for SAR4, the RLAN2 high speed W
22、LAN transmitter interference was above the acceptable levels for both SAR3 and SAR4, and the RLAN3 high speed WLAN transmitter interference was above the acceptable level for SAR4. For indoors/outdoors RLAN deployment, it is feasible for the RLAN1, based on an assumption of only 12 active transmitte
23、rs per km2within the Parameter Value Antenna gain (dBi) 31 (mid) 28.5 (mid) 32.5 (fore/aft) 29.5 (fore/aft) Antenna mainbeam orientation (degrees) Incidence angles: 18-47 (mid) 24-57 (fore/aft) Incidence angles: 25.0-54.5 (mid) 33.7-65.3 (fore/aft) Antenna beamwidth (3 dB), elevation Azimuth beamwid
24、th 24 (mid) 1.3 26 (fore/aft) 0.8 23.6 (mid) 1.1 23.9 (fore/aft) 0.8 Instrument elevation angle (degrees) 29.3 37.6 Antenna polarization Vertical Vertical Transmitter peak power 4.8 kW 120 W Receiver noise temperature (dB) Noise factor: 3 Noise factor: 3 Service area Oceanic and coastal areas, land
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